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You searched for subject:(Attitude estimation). Showing records 1 – 30 of 66 total matches.

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Texas A&M University

1. Swanzy, Michael John. Analysis and demonstration: a proof-of-concept compass star tracker.

Degree: 2007, Texas A&M University

 This research analyzes and demonstrates the local position determination problem on Earth using a novel instrument, the Compass Star Tracker. Special focus is given to… (more)

Subjects/Keywords: Navigation; Attitude Estimation

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Swanzy, M. J. (2007). Analysis and demonstration: a proof-of-concept compass star tracker. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4853

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Swanzy, Michael John. “Analysis and demonstration: a proof-of-concept compass star tracker.” 2007. Thesis, Texas A&M University. Accessed January 19, 2020. http://hdl.handle.net/1969.1/4853.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Swanzy, Michael John. “Analysis and demonstration: a proof-of-concept compass star tracker.” 2007. Web. 19 Jan 2020.

Vancouver:

Swanzy MJ. Analysis and demonstration: a proof-of-concept compass star tracker. [Internet] [Thesis]. Texas A&M University; 2007. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/1969.1/4853.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Swanzy MJ. Analysis and demonstration: a proof-of-concept compass star tracker. [Thesis]. Texas A&M University; 2007. Available from: http://hdl.handle.net/1969.1/4853

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

2. Ibrahim, Najmus. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.

Degree: 2013, University of Toronto

Terrestrial target tracking using low Earth orbit satellites provides essential daily services and vital scientific data. In this thesis, the Attitude and Orbit Control System… (more)

Subjects/Keywords: satellite; attitude; attitude and orbit control; microsatellite; control; estimation; tracking; 0538

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ibrahim, N. (2013). Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/42965

Chicago Manual of Style (16th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Masters Thesis, University of Toronto. Accessed January 19, 2020. http://hdl.handle.net/1807/42965.

MLA Handbook (7th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Web. 19 Jan 2020.

Vancouver:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/1807/42965.

Council of Science Editors:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42965


Rochester Institute of Technology

3. Scorse, William. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.

Degree: Mechanical Engineering, 2011, Rochester Institute of Technology

 In this thesis, a previously developed, novel one-dimensional attitude estimation device is expanded through the development and implementation of an innovative method for estimation of… (more)

Subjects/Keywords: Attitude estimation; Bias estimation; Euler kinematics; Kalman filtering; Rigid body dynamics

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APA (6th Edition):

Scorse, W. (2011). Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5803

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Scorse, William. “Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.” 2011. Thesis, Rochester Institute of Technology. Accessed January 19, 2020. https://scholarworks.rit.edu/theses/5803.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Scorse, William. “Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.” 2011. Web. 19 Jan 2020.

Vancouver:

Scorse W. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. [Internet] [Thesis]. Rochester Institute of Technology; 2011. [cited 2020 Jan 19]. Available from: https://scholarworks.rit.edu/theses/5803.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Scorse W. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. [Thesis]. Rochester Institute of Technology; 2011. Available from: https://scholarworks.rit.edu/theses/5803

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

4. Vivek Chandran, K P. Development Of Gyroless Attitude And Angular Rate Estimation For Satellites.

Degree: 2009, Indian Institute of Science

 Studies aimed at the development of indigenous low cost star tracker and gyroless attitude and angular rate estimation is presented in the thesis. This study… (more)

Subjects/Keywords: Gyroless Attitude; Satellites - Angular Rate; Star Trackers; Satellites - Attitude Estimation; Star Sensors; Stars - Catalogs; Satellite Attitude Control; Gyroless Satellite Attitude Estimation; Angular Rate Estimation; Micro-Satellites; Astronautics

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APA (6th Edition):

Vivek Chandran, K. P. (2009). Development Of Gyroless Attitude And Angular Rate Estimation For Satellites. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1121

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Vivek Chandran, K P. “Development Of Gyroless Attitude And Angular Rate Estimation For Satellites.” 2009. Thesis, Indian Institute of Science. Accessed January 19, 2020. http://hdl.handle.net/2005/1121.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Vivek Chandran, K P. “Development Of Gyroless Attitude And Angular Rate Estimation For Satellites.” 2009. Web. 19 Jan 2020.

Vancouver:

Vivek Chandran KP. Development Of Gyroless Attitude And Angular Rate Estimation For Satellites. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/2005/1121.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Vivek Chandran KP. Development Of Gyroless Attitude And Angular Rate Estimation For Satellites. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1121

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

5. Benziane, Lotfi. Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles.

Degree: Docteur es, Informatique, 2015, Versailles-St Quentin en Yvelines

Les drones ou systèmes de drones aériens jouent un rôle de plus en plus important danstous les domaines, spécialement les drones à décollage et atterrissage… (more)

Subjects/Keywords: Estimation de l'attitude; Filtres complémentaires; Attitude estimation; Complementary filter; Aerial vehicle; Imu; Attitude control; Data fusion; Quadcopter

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Benziane, L. (2015). Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles. (Doctoral Dissertation). Versailles-St Quentin en Yvelines. Retrieved from http://www.theses.fr/2015VERS015V

Chicago Manual of Style (16th Edition):

Benziane, Lotfi. “Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles.” 2015. Doctoral Dissertation, Versailles-St Quentin en Yvelines. Accessed January 19, 2020. http://www.theses.fr/2015VERS015V.

MLA Handbook (7th Edition):

Benziane, Lotfi. “Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles.” 2015. Web. 19 Jan 2020.

Vancouver:

Benziane L. Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles. [Internet] [Doctoral dissertation]. Versailles-St Quentin en Yvelines; 2015. [cited 2020 Jan 19]. Available from: http://www.theses.fr/2015VERS015V.

Council of Science Editors:

Benziane L. Contributions à l'estimation et à la commande d'attitude de véhicules aériens autonomes : Attitude estimation & control of autonomous aerial vehicles. [Doctoral Dissertation]. Versailles-St Quentin en Yvelines; 2015. Available from: http://www.theses.fr/2015VERS015V


Queensland University of Technology

6. Dusha, Damien. Integrated vision-based attitude estimation.

Degree: 2012, Queensland University of Technology

 For many years, computer vision has lured researchers with promises of a low-cost, passive, lightweight and information-rich sensor suitable for navigation purposes. The prime difficulty… (more)

Subjects/Keywords: integrated vision-based attitude estimation; horizon-detection algorithm

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Dusha, D. (2012). Integrated vision-based attitude estimation. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/51558/

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Dusha, Damien. “Integrated vision-based attitude estimation.” 2012. Thesis, Queensland University of Technology. Accessed January 19, 2020. https://eprints.qut.edu.au/51558/.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Dusha, Damien. “Integrated vision-based attitude estimation.” 2012. Web. 19 Jan 2020.

Vancouver:

Dusha D. Integrated vision-based attitude estimation. [Internet] [Thesis]. Queensland University of Technology; 2012. [cited 2020 Jan 19]. Available from: https://eprints.qut.edu.au/51558/.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Dusha D. Integrated vision-based attitude estimation. [Thesis]. Queensland University of Technology; 2012. Available from: https://eprints.qut.edu.au/51558/

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Brno University of Technology

7. Baránek, Radek. Estimace orientace multikoptér .

Degree: 2015, Brno University of Technology

 Tato dizertační práce se zabývá estimací orientace multikoptér. Především je zkoumáno zahrnutí dynamického modelu multikoptéry do estimačního algoritmu za účelem zpřesnění odhadnuté orientace. Ukazuje se,… (more)

Subjects/Keywords: Estimace orientace; Multikoptéry; Kalmanův filtr; Attitude estimation; Multicopters; Kalman filter

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APA (6th Edition):

Baránek, R. (2015). Estimace orientace multikoptér . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/51727

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Baránek, Radek. “Estimace orientace multikoptér .” 2015. Thesis, Brno University of Technology. Accessed January 19, 2020. http://hdl.handle.net/11012/51727.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Baránek, Radek. “Estimace orientace multikoptér .” 2015. Web. 19 Jan 2020.

Vancouver:

Baránek R. Estimace orientace multikoptér . [Internet] [Thesis]. Brno University of Technology; 2015. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/11012/51727.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Baránek R. Estimace orientace multikoptér . [Thesis]. Brno University of Technology; 2015. Available from: http://hdl.handle.net/11012/51727

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Queensland University of Technology

8. Dando, Aaron John. Robust adaptive control of rigid spacecraft attitude maneuvers.

Degree: 2008, Queensland University of Technology

 In this thesis novel feedback attitude control algorithms and attitude estimation algorithms are developed for a three-axis stabilised spacecraft attitude control system. The spacecraft models… (more)

Subjects/Keywords: spacecraft attitude control system; spacecraft attitude manevers; spacecraft attitude estimation; Lyapunov stability theory; adaptive control theory; optimal control theory; state estimation theory

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APA (6th Edition):

Dando, A. J. (2008). Robust adaptive control of rigid spacecraft attitude maneuvers. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/16695/

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Dando, Aaron John. “Robust adaptive control of rigid spacecraft attitude maneuvers.” 2008. Thesis, Queensland University of Technology. Accessed January 19, 2020. https://eprints.qut.edu.au/16695/.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Dando, Aaron John. “Robust adaptive control of rigid spacecraft attitude maneuvers.” 2008. Web. 19 Jan 2020.

Vancouver:

Dando AJ. Robust adaptive control of rigid spacecraft attitude maneuvers. [Internet] [Thesis]. Queensland University of Technology; 2008. [cited 2020 Jan 19]. Available from: https://eprints.qut.edu.au/16695/.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Dando AJ. Robust adaptive control of rigid spacecraft attitude maneuvers. [Thesis]. Queensland University of Technology; 2008. Available from: https://eprints.qut.edu.au/16695/

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of California – Berkeley

9. Wang, Yizhou. Attitude Control and Estimation.

Degree: Mechanical Engineering, 2015, University of California – Berkeley

 The attitude control problem, or the control of a spacecraft's orientation with respect to a frame of reference, is a challenging problem in space missions… (more)

Subjects/Keywords: Mechanical engineering; Aerospace engineering; Adaptive control; Attitude control; Attitude estimation; IMU; Particle filter; Sliding mode control

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APA (6th Edition):

Wang, Y. (2015). Attitude Control and Estimation. (Thesis). University of California – Berkeley. Retrieved from http://www.escholarship.org/uc/item/59b5d7hh

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wang, Yizhou. “Attitude Control and Estimation.” 2015. Thesis, University of California – Berkeley. Accessed January 19, 2020. http://www.escholarship.org/uc/item/59b5d7hh.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wang, Yizhou. “Attitude Control and Estimation.” 2015. Web. 19 Jan 2020.

Vancouver:

Wang Y. Attitude Control and Estimation. [Internet] [Thesis]. University of California – Berkeley; 2015. [cited 2020 Jan 19]. Available from: http://www.escholarship.org/uc/item/59b5d7hh.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wang Y. Attitude Control and Estimation. [Thesis]. University of California – Berkeley; 2015. Available from: http://www.escholarship.org/uc/item/59b5d7hh

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Université de Grenoble

10. Nguyen, Hoang Van. Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities.

Degree: Docteur es, Automatique et productique, 2011, Université de Grenoble

L'estimation de l'attitude (ou orientation) est un problème récurrent de nombreuses applications allant de la robotique aérienne ou sous-marine en passant par des applications médicales… (more)

Subjects/Keywords: Estimation d'attitude; Estimation ensembliste; Diagnostic ensembliste; Centrale inertielle; Imu; Fdi; Attitude estimation; Set-membership estimation; Set-membership diagnosis; Inertial measurement unit; Imu; Fdi; 620

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APA (6th Edition):

Nguyen, H. V. (2011). Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities. (Doctoral Dissertation). Université de Grenoble. Retrieved from http://www.theses.fr/2011GRENT011

Chicago Manual of Style (16th Edition):

Nguyen, Hoang Van. “Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities.” 2011. Doctoral Dissertation, Université de Grenoble. Accessed January 19, 2020. http://www.theses.fr/2011GRENT011.

MLA Handbook (7th Edition):

Nguyen, Hoang Van. “Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities.” 2011. Web. 19 Jan 2020.

Vancouver:

Nguyen HV. Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities. [Internet] [Doctoral dissertation]. Université de Grenoble; 2011. [cited 2020 Jan 19]. Available from: http://www.theses.fr/2011GRENT011.

Council of Science Editors:

Nguyen HV. Estimation d'attitude et diagnostic d'une centrale d'attitude par des outils ensemblistes : Attitude central unit with accurate computation of the attitude and sensor fault detection capabilities. [Doctoral Dissertation]. Université de Grenoble; 2011. Available from: http://www.theses.fr/2011GRENT011


Rochester Institute of Technology

11. Weisman, Ryan. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.

Degree: Mechanical Engineering, 2008, Rochester Institute of Technology

 In this thesis, a novel attitude estimation device is proposed utilizing cost-effective measurement sensors. The device fuses a rate gyroscope with an accelerometer array to… (more)

Subjects/Keywords: Attitude estimation; Bias estimation; Kalman filtering; Rigid body dynamics

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APA (6th Edition):

Weisman, R. (2008). Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5807

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Weisman, Ryan. “Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.” 2008. Thesis, Rochester Institute of Technology. Accessed January 19, 2020. https://scholarworks.rit.edu/theses/5807.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Weisman, Ryan. “Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.” 2008. Web. 19 Jan 2020.

Vancouver:

Weisman R. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. [Internet] [Thesis]. Rochester Institute of Technology; 2008. [cited 2020 Jan 19]. Available from: https://scholarworks.rit.edu/theses/5807.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Weisman R. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. [Thesis]. Rochester Institute of Technology; 2008. Available from: https://scholarworks.rit.edu/theses/5807

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Rochester Institute of Technology

12. Szklany, Steven. A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation.

Degree: Mechanical Engineering, 2012, Rochester Institute of Technology

 In this work, a highly accurate navigation device is proposed for unmanned underwater vehicle navigation. A six degree of freedom, open loop underwater vehicle model… (more)

Subjects/Keywords: Adaptive gain sliding mode control; Attitude estimation; Sliding mode differentiation; Underwater vehicle navigation

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APA (6th Edition):

Szklany, S. (2012). A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5805

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Szklany, Steven. “A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation.” 2012. Thesis, Rochester Institute of Technology. Accessed January 19, 2020. https://scholarworks.rit.edu/theses/5805.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Szklany, Steven. “A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation.” 2012. Web. 19 Jan 2020.

Vancouver:

Szklany S. A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation. [Internet] [Thesis]. Rochester Institute of Technology; 2012. [cited 2020 Jan 19]. Available from: https://scholarworks.rit.edu/theses/5805.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Szklany S. A Feasibility assessment of a new navigation system for unmanned underwater vehicles with adaptive gain sliding mode differentiation. [Thesis]. Rochester Institute of Technology; 2012. Available from: https://scholarworks.rit.edu/theses/5805

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Penn State University

13. Proffitt, Richard P. Vision based map-to-image correspondence for attitude estimation in augmented reality applications.

Degree: PhD, Mechanical Engineering, 2016, Penn State University

 This dissertation proposes a methodology for attitude correction by matching two different representations of the same environment. This is accomplished by matching features extracted from… (more)

Subjects/Keywords: Augmented reality; horizon matching; sequence matching; vision-based attitude estimation; sensor fusion; visual navigation

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APA (6th Edition):

Proffitt, R. P. (2016). Vision based map-to-image correspondence for attitude estimation in augmented reality applications. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/28856

Chicago Manual of Style (16th Edition):

Proffitt, Richard P. “Vision based map-to-image correspondence for attitude estimation in augmented reality applications.” 2016. Doctoral Dissertation, Penn State University. Accessed January 19, 2020. https://etda.libraries.psu.edu/catalog/28856.

MLA Handbook (7th Edition):

Proffitt, Richard P. “Vision based map-to-image correspondence for attitude estimation in augmented reality applications.” 2016. Web. 19 Jan 2020.

Vancouver:

Proffitt RP. Vision based map-to-image correspondence for attitude estimation in augmented reality applications. [Internet] [Doctoral dissertation]. Penn State University; 2016. [cited 2020 Jan 19]. Available from: https://etda.libraries.psu.edu/catalog/28856.

Council of Science Editors:

Proffitt RP. Vision based map-to-image correspondence for attitude estimation in augmented reality applications. [Doctoral Dissertation]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/28856


University of California – Santa Cruz

14. Eliahu, Daniel Shalom. Classification, Tracking, and Suppression of Parkinsonian Tremor.

Degree: Computer Engineering (Robotics and Control), 2017, University of California – Santa Cruz

 Approximately 11 million Americans live with Parkinson’s Disease (PD) or Essential Tremor (ET), and the current standard of care is inadequate. Diagnostic methods rely on… (more)

Subjects/Keywords: Robotics; Computer engineering; Neurosciences; Attitude Estimation; Essential Tremor; Exoskeleton; Parkinson's Disease; Tremor Diagnosis; Tremor Suppression

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APA (6th Edition):

Eliahu, D. S. (2017). Classification, Tracking, and Suppression of Parkinsonian Tremor. (Thesis). University of California – Santa Cruz. Retrieved from http://www.escholarship.org/uc/item/8qm3m3v8

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Eliahu, Daniel Shalom. “Classification, Tracking, and Suppression of Parkinsonian Tremor.” 2017. Thesis, University of California – Santa Cruz. Accessed January 19, 2020. http://www.escholarship.org/uc/item/8qm3m3v8.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Eliahu, Daniel Shalom. “Classification, Tracking, and Suppression of Parkinsonian Tremor.” 2017. Web. 19 Jan 2020.

Vancouver:

Eliahu DS. Classification, Tracking, and Suppression of Parkinsonian Tremor. [Internet] [Thesis]. University of California – Santa Cruz; 2017. [cited 2020 Jan 19]. Available from: http://www.escholarship.org/uc/item/8qm3m3v8.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Eliahu DS. Classification, Tracking, and Suppression of Parkinsonian Tremor. [Thesis]. University of California – Santa Cruz; 2017. Available from: http://www.escholarship.org/uc/item/8qm3m3v8

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

15. Cratty, Krista. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 Sting-mounted models that undergo significant unsteady motion suffer from degraded data quality because the data is time-averaged to remove the unsteady fluctuations. However, time-averaged data… (more)

Subjects/Keywords: State Estimation; Wind Tunnel; Wind Tunnel Measurements; WB-57; Model Attitude; Kalman Filter

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APA (6th Edition):

Cratty, K. (2017). Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169617

Chicago Manual of Style (16th Edition):

Cratty, Krista. “Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.” 2017. Masters Thesis, Texas A&M University. Accessed January 19, 2020. http://hdl.handle.net/1969.1/169617.

MLA Handbook (7th Edition):

Cratty, Krista. “Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.” 2017. Web. 19 Jan 2020.

Vancouver:

Cratty K. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/1969.1/169617.

Council of Science Editors:

Cratty K. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169617


University of Waterloo

16. Koldychev, Mikhail. Observers on linear Lie groups with linear estimation error dynamics.

Degree: 2012, University of Waterloo

 A major motivation for Lie group observers is their application as sensor fusion algorithms for an inertial measurement unit which can be used to estimate… (more)

Subjects/Keywords: observer; lie group; high-gain observer; inertial measurement; attitude estimation; linear error dynamics

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APA (6th Edition):

Koldychev, M. (2012). Observers on linear Lie groups with linear estimation error dynamics. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/7001

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Koldychev, Mikhail. “Observers on linear Lie groups with linear estimation error dynamics.” 2012. Thesis, University of Waterloo. Accessed January 19, 2020. http://hdl.handle.net/10012/7001.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Koldychev, Mikhail. “Observers on linear Lie groups with linear estimation error dynamics.” 2012. Web. 19 Jan 2020.

Vancouver:

Koldychev M. Observers on linear Lie groups with linear estimation error dynamics. [Internet] [Thesis]. University of Waterloo; 2012. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/10012/7001.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Koldychev M. Observers on linear Lie groups with linear estimation error dynamics. [Thesis]. University of Waterloo; 2012. Available from: http://hdl.handle.net/10012/7001

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Luleå University of Technology

17. Schiemenz, Fabian. Spacecraft Attitude Estimation Under Agility Constraints.

Degree: 2015, Luleå University of Technology

Agility describes the ability of a spacecraft to arbitrarily and rapidly reorient itself inspace. In recent years the desire for increased agility has turned… (more)

Subjects/Keywords: Technology; Attitude Estimation; Agility; Kalman Filter; Gyro-Calibration; Nullspace updates; Observability; Calibration Maneuvers; Teknik

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APA (6th Edition):

Schiemenz, F. (2015). Spacecraft Attitude Estimation Under Agility Constraints. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56005

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Schiemenz, Fabian. “Spacecraft Attitude Estimation Under Agility Constraints.” 2015. Thesis, Luleå University of Technology. Accessed January 19, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56005.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Schiemenz, Fabian. “Spacecraft Attitude Estimation Under Agility Constraints.” 2015. Web. 19 Jan 2020.

Vancouver:

Schiemenz F. Spacecraft Attitude Estimation Under Agility Constraints. [Internet] [Thesis]. Luleå University of Technology; 2015. [cited 2020 Jan 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56005.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Schiemenz F. Spacecraft Attitude Estimation Under Agility Constraints. [Thesis]. Luleå University of Technology; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56005

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

18. Bergman, Kristoffer. Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques.

Degree: The Institute of Technology, 2014, Linköping UniversityLinköping University

A multirotor is a type of aerial vehicle that has attracted a lot of attention in recent years. Multirotors have found applications in a… (more)

Subjects/Keywords: Multirotor; Octorotor; VTOL; UAV; Modeling; Estimation; Attitude control; PID; L1 adaptive control

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APA (6th Edition):

Bergman, K. (2014). Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques. (Thesis). Linköping UniversityLinköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-107562

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bergman, Kristoffer. “Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques.” 2014. Thesis, Linköping UniversityLinköping University. Accessed January 19, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-107562.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bergman, Kristoffer. “Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques.” 2014. Web. 19 Jan 2020.

Vancouver:

Bergman K. Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques. [Internet] [Thesis]. Linköping UniversityLinköping University; 2014. [cited 2020 Jan 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-107562.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bergman K. Modeling, Estimation and Attitude Control of an Octorotor Using PID and L1 Adaptive Control Techniques. [Thesis]. Linköping UniversityLinköping University; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-107562

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Texas – Austin

19. -7636-3233. An attitude determination and control system for small satellites.

Degree: MSin Engineering, Aerospace Engineering, 2015, University of Texas – Austin

 A flexible, robust attitude determination and control (ADC) system is presented for small satellite platforms. Using commercial-off-the-shelf sensors, reaction wheels, and magnetorquers which fit within… (more)

Subjects/Keywords: Attitude; Determination; Control; Estimation; CubeSat; Satellite; ADC; Guidance; Convex optimization; Constrained attitude guidance; Attitude constraint; Texas Spacecraft Laboratory; TSL; Bevo-2; ARMADILLO

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APA (6th Edition):

-7636-3233. (2015). An attitude determination and control system for small satellites. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31715

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Masters Thesis, University of Texas – Austin. Accessed January 19, 2020. http://hdl.handle.net/2152/31715.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Web. 19 Jan 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-7636-3233. An attitude determination and control system for small satellites. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/2152/31715.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-7636-3233. An attitude determination and control system for small satellites. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31715

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Indian Institute of Science

20. Pal, Madhumita. Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation.

Degree: 2013, Indian Institute of Science

 This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and attitude rate. The main objective of this thesis is to explore the possibility of… (more)

Subjects/Keywords: Gyroless Micro-Satellite Attitude; Micro-satellite Attitude; Micro-Satellite Attitude Determination; Micro-Light Star Sensors; Second Order Sliding Mode Observer (SOSMO); Satellite Angular Rate Estimation; Spacecraft Attitude Determination; Gyroless Angular Rate Estimatiom; Star Sensor based Satellite Attitude Rate Estimation; Micro-Satellites; Star Tracker; Star Sensor Micro-Satellite Attitude - Alogorithms; Linear Multi Output System; Micro-Satellite Angular Rate Estimation; Star Camera Calibration; Aerospace Engineering

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APA (6th Edition):

Pal, M. (2013). Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3428 ; http://etd.iisc.ernet.in/abstracts/4295/G25940-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Pal, Madhumita. “Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation.” 2013. Thesis, Indian Institute of Science. Accessed January 19, 2020. http://etd.iisc.ernet.in/2005/3428 ; http://etd.iisc.ernet.in/abstracts/4295/G25940-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Pal, Madhumita. “Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation.” 2013. Web. 19 Jan 2020.

Vancouver:

Pal M. Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2020 Jan 19]. Available from: http://etd.iisc.ernet.in/2005/3428 ; http://etd.iisc.ernet.in/abstracts/4295/G25940-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Pal M. Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation. [Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ernet.in/2005/3428 ; http://etd.iisc.ernet.in/abstracts/4295/G25940-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of New South Wales

21. Habibi Tehrani, Mohsen. Aircraft Attitude Estimation Using Panoramic Images.

Degree: Engineering & Information Technology Canberra, 2014, University of New South Wales

 This thesis investigates the problem of reliably estimating attitude from panoramic imagery in cluttered environments. Accurate attitude is an essential input to the stabilisation systems… (more)

Subjects/Keywords: Aircraft Attitude Estimation; Panoramic Images; Estimating attitude; Cluttered environments; Ocelli organ; Real–; time horizon-based attitude estimation; Panoramic sky/ground thresholding; Three–; dimensional mapping; Image interpolation algorithm (I2A); Extended Kalman Filter (EKF); Artificial Neural Networks (ANNs); Flight tests

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APA (6th Edition):

Habibi Tehrani, M. (2014). Aircraft Attitude Estimation Using Panoramic Images. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/54009 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12717/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Habibi Tehrani, Mohsen. “Aircraft Attitude Estimation Using Panoramic Images.” 2014. Doctoral Dissertation, University of New South Wales. Accessed January 19, 2020. http://handle.unsw.edu.au/1959.4/54009 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12717/SOURCE02?view=true.

MLA Handbook (7th Edition):

Habibi Tehrani, Mohsen. “Aircraft Attitude Estimation Using Panoramic Images.” 2014. Web. 19 Jan 2020.

Vancouver:

Habibi Tehrani M. Aircraft Attitude Estimation Using Panoramic Images. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2020 Jan 19]. Available from: http://handle.unsw.edu.au/1959.4/54009 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12717/SOURCE02?view=true.

Council of Science Editors:

Habibi Tehrani M. Aircraft Attitude Estimation Using Panoramic Images. [Doctoral Dissertation]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/54009 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12717/SOURCE02?view=true


University of Western Ontario

22. Berkane, Soulaimane. Hybrid Attitude Control and Estimation On SO(3).

Degree: 2017, University of Western Ontario

 This thesis presents a general framework for hybrid attitude control and estimation design on the Special Orthogonal group SO(3). First, the attitude stabilization problem on… (more)

Subjects/Keywords: Attitude control; Attitude estimation; Hybrid systems; Special Orthogonal group; Intermittent measurements; synergistic hybrid feedback; Acoustics, Dynamics, and Controls; Aerospace Engineering; Controls and Control Theory; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Berkane, S. (2017). Hybrid Attitude Control and Estimation On SO(3). (Thesis). University of Western Ontario. Retrieved from https://ir.lib.uwo.ca/etd/5083

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Berkane, Soulaimane. “Hybrid Attitude Control and Estimation On SO(3).” 2017. Thesis, University of Western Ontario. Accessed January 19, 2020. https://ir.lib.uwo.ca/etd/5083.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Berkane, Soulaimane. “Hybrid Attitude Control and Estimation On SO(3).” 2017. Web. 19 Jan 2020.

Vancouver:

Berkane S. Hybrid Attitude Control and Estimation On SO(3). [Internet] [Thesis]. University of Western Ontario; 2017. [cited 2020 Jan 19]. Available from: https://ir.lib.uwo.ca/etd/5083.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Berkane S. Hybrid Attitude Control and Estimation On SO(3). [Thesis]. University of Western Ontario; 2017. Available from: https://ir.lib.uwo.ca/etd/5083

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Universidade do Rio Grande do Norte

23. Sanca, Armando Sanca. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .

Degree: 2013, Universidade do Rio Grande do Norte

 In this Thesis, the development of the dynamic model of multirotor unmanned aerial vehicle with vertical takeoff and landing characteristics, considering input nonlinearities and a… (more)

Subjects/Keywords: Hexarrotor. Modelagem Dinâmica. Controle robusto por backstepping. Estimação de atitude por FKE; Hexarotor. Dynamic modeling. Robust backstepping control. EKF Attitude Estimation

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APA (6th Edition):

Sanca, A. S. (2013). Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . (Doctoral Dissertation). Universidade do Rio Grande do Norte. Retrieved from http://repositorio.ufrn.br/handle/123456789/15220

Chicago Manual of Style (16th Edition):

Sanca, Armando Sanca. “Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .” 2013. Doctoral Dissertation, Universidade do Rio Grande do Norte. Accessed January 19, 2020. http://repositorio.ufrn.br/handle/123456789/15220.

MLA Handbook (7th Edition):

Sanca, Armando Sanca. “Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .” 2013. Web. 19 Jan 2020.

Vancouver:

Sanca AS. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . [Internet] [Doctoral dissertation]. Universidade do Rio Grande do Norte; 2013. [cited 2020 Jan 19]. Available from: http://repositorio.ufrn.br/handle/123456789/15220.

Council of Science Editors:

Sanca AS. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . [Doctoral Dissertation]. Universidade do Rio Grande do Norte; 2013. Available from: http://repositorio.ufrn.br/handle/123456789/15220


Universidade do Rio Grande do Norte

24. Sanca, Armando Sanca. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .

Degree: 2013, Universidade do Rio Grande do Norte

 In this Thesis, the development of the dynamic model of multirotor unmanned aerial vehicle with vertical takeoff and landing characteristics, considering input nonlinearities and a… (more)

Subjects/Keywords: Hexarrotor. Modelagem Dinâmica. Controle robusto por backstepping. Estimação de atitude por FKE; Hexarotor. Dynamic modeling. Robust backstepping control. EKF Attitude Estimation

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APA (6th Edition):

Sanca, A. S. (2013). Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . (Thesis). Universidade do Rio Grande do Norte. Retrieved from http://repositorio.ufrn.br/handle/123456789/15220

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sanca, Armando Sanca. “Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .” 2013. Thesis, Universidade do Rio Grande do Norte. Accessed January 19, 2020. http://repositorio.ufrn.br/handle/123456789/15220.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sanca, Armando Sanca. “Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor .” 2013. Web. 19 Jan 2020.

Vancouver:

Sanca AS. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . [Internet] [Thesis]. Universidade do Rio Grande do Norte; 2013. [cited 2020 Jan 19]. Available from: http://repositorio.ufrn.br/handle/123456789/15220.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sanca AS. Modelagem e controle de um microveículo aéreo: uma aplicação de estabilidade robusta com a técnica backstepping em uma estrutura hexarrotor . [Thesis]. Universidade do Rio Grande do Norte; 2013. Available from: http://repositorio.ufrn.br/handle/123456789/15220

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Ohio University

25. Sabala, Ryan J. Satellite Attitude Determination Using Laser Communication Systems.

Degree: MS, Electrical Engineering (Engineering and Technology), 2008, Ohio University

 Satellite laser communication systems provide measurements that can be further processed to provide relative attitude estimates of each satellite in the constellation. This suggests a… (more)

Subjects/Keywords: Electrical Engineering; Satellite Attitude Determination; Laser Communication System; Satellite Laser Communication; Sensitivity Analysis; Static Estimation; Error Sources

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APA (6th Edition):

Sabala, R. J. (2008). Satellite Attitude Determination Using Laser Communication Systems. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1218636153

Chicago Manual of Style (16th Edition):

Sabala, Ryan J. “Satellite Attitude Determination Using Laser Communication Systems.” 2008. Masters Thesis, Ohio University. Accessed January 19, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1218636153.

MLA Handbook (7th Edition):

Sabala, Ryan J. “Satellite Attitude Determination Using Laser Communication Systems.” 2008. Web. 19 Jan 2020.

Vancouver:

Sabala RJ. Satellite Attitude Determination Using Laser Communication Systems. [Internet] [Masters thesis]. Ohio University; 2008. [cited 2020 Jan 19]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1218636153.

Council of Science Editors:

Sabala RJ. Satellite Attitude Determination Using Laser Communication Systems. [Masters Thesis]. Ohio University; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1218636153


Brigham Young University

26. Chamberlain, Caleb H. System Identification, State Estimation, and Control of Unmanned Aerial Robots.

Degree: MS, 2011, Brigham Young University

  This thesis describes work in a variety of topics related to aerial robotics, including system identification, state estimation, control, and path planning. The path… (more)

Subjects/Keywords: quadrotor control; path planning; aerial surveillance; system identification; quadrotor attitude estimation; quadrotor; Electrical and Computer Engineering

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APA (6th Edition):

Chamberlain, C. H. (2011). System Identification, State Estimation, and Control of Unmanned Aerial Robots. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3604&context=etd

Chicago Manual of Style (16th Edition):

Chamberlain, Caleb H. “System Identification, State Estimation, and Control of Unmanned Aerial Robots.” 2011. Masters Thesis, Brigham Young University. Accessed January 19, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3604&context=etd.

MLA Handbook (7th Edition):

Chamberlain, Caleb H. “System Identification, State Estimation, and Control of Unmanned Aerial Robots.” 2011. Web. 19 Jan 2020.

Vancouver:

Chamberlain CH. System Identification, State Estimation, and Control of Unmanned Aerial Robots. [Internet] [Masters thesis]. Brigham Young University; 2011. [cited 2020 Jan 19]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3604&context=etd.

Council of Science Editors:

Chamberlain CH. System Identification, State Estimation, and Control of Unmanned Aerial Robots. [Masters Thesis]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3604&context=etd


University of California – Santa Cruz

27. LISS, JORDAN A. Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter.

Degree: Computer Engineering (Robotics and Control), 2018, University of California – Santa Cruz

 Very small spacecraft, called SmallSats, CubeSats, and NanoSats, have become very popular due to their low-cost, complexity, and availability of launch platforms (as extra payloads).… (more)

Subjects/Keywords: Computer engineering; Robotics; Aerospace engineering; AprilTag; Attitude Estimation; Computer Vision; CubeSat; Extended Kalman Filters; Sensor Fusion

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

LISS, J. A. (2018). Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter. (Thesis). University of California – Santa Cruz. Retrieved from http://www.escholarship.org/uc/item/04n983jj

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

LISS, JORDAN A. “Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter.” 2018. Thesis, University of California – Santa Cruz. Accessed January 19, 2020. http://www.escholarship.org/uc/item/04n983jj.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

LISS, JORDAN A. “Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter.” 2018. Web. 19 Jan 2020.

Vancouver:

LISS JA. Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter. [Internet] [Thesis]. University of California – Santa Cruz; 2018. [cited 2020 Jan 19]. Available from: http://www.escholarship.org/uc/item/04n983jj.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

LISS JA. Verification of TRIAD and Complementary Filter on CubeSat using Low-Cost Extrinsic Visual Marker Tracking with an Extended Kalman Filter. [Thesis]. University of California – Santa Cruz; 2018. Available from: http://www.escholarship.org/uc/item/04n983jj

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of New South Wales

28. Del Rosario, Michael. Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation.

Degree: Graduate School of Biomedical Engineering, 2017, University of New South Wales

 Completing a cardiac rehabilitation program (CRP) following myocardial infarction has many health benefits, but CRP is not completed by all patients. This thesis investigated if… (more)

Subjects/Keywords: Cardiac rehabilitation; Smartphone; Near field communication; Attitude estimation; Human activity classification; mHealth; Accelerometer; Gyroscope; Magnetometer; Barometer

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Del Rosario, M. (2017). Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/58220 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45601/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Del Rosario, Michael. “Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation.” 2017. Doctoral Dissertation, University of New South Wales. Accessed January 19, 2020. http://handle.unsw.edu.au/1959.4/58220 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45601/SOURCE02?view=true.

MLA Handbook (7th Edition):

Del Rosario, Michael. “Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation.” 2017. Web. 19 Jan 2020.

Vancouver:

Del Rosario M. Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2020 Jan 19]. Available from: http://handle.unsw.edu.au/1959.4/58220 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45601/SOURCE02?view=true.

Council of Science Editors:

Del Rosario M. Convergence of smartphone technology and algorithms that estimate physical activity for cardiac rehabilitation. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/58220 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45601/SOURCE02?view=true


KTH

29. Jéger, Csaba. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.

Degree: Space and Plasma Physics, 2017, KTH

SEAM (Small Explorer for Advanced Missions) is a 3U CubeSat developedat KTH Royal Institute of Technology which will provide highqualityDC and AC magnetic field… (more)

Subjects/Keywords: cubesat; magnetic dipole estimation; attitude dynamics; cubesat; magnetisk dipol uppskattning; attityddynamik; Electrical Engineering, Electronic Engineering, Information Engineering; Elektroteknik och elektronik

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Jéger, C. (2017). Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Jéger, Csaba. “Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.” 2017. Thesis, KTH. Accessed January 19, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Jéger, Csaba. “Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.” 2017. Web. 19 Jan 2020.

Vancouver:

Jéger C. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. [Internet] [Thesis]. KTH; 2017. [cited 2020 Jan 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jéger C. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. [Thesis]. KTH; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

30. Ainscough, Thomas. Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter.

Degree: MS, Engineering, 2013, Rice University

 A new algorithm is proposed that smoothly integrates the nonlinear estimation of the attitude quaternion using Davenport's q-method and the estimation of non-attitude states within… (more)

Subjects/Keywords: Attitude estimation; Nonlinear estimation; Extended Kalman filter; Wahba problem

…11 4.1 Attitude Estimation Error 100 Run Monte Carlo . . . . . . . . . . . . 71 4.2… …Gyro Bias Estimation Error 100 Run Monte Carlo . . . . . . . . . . . 72 4.3 Attitude… …75 4.5 Attitude Estimation Error for Eclipse 100 Run Monte Carlo . . . . . 77 4.6 Gyro… …Bias Estimation Error for Eclipse 100 Run Monte Carlo . . . . 77 4.7 Attitude Estimation… …accurate attitude estimation is essential for the primary mission objective such as in remote… 

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ainscough, T. (2013). Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/71913

Chicago Manual of Style (16th Edition):

Ainscough, Thomas. “Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter.” 2013. Masters Thesis, Rice University. Accessed January 19, 2020. http://hdl.handle.net/1911/71913.

MLA Handbook (7th Edition):

Ainscough, Thomas. “Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter.” 2013. Web. 19 Jan 2020.

Vancouver:

Ainscough T. Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter. [Internet] [Masters thesis]. Rice University; 2013. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/1911/71913.

Council of Science Editors:

Ainscough T. Spacecraft Attitude Estimation Integrating the Q-Method into an Extended Kalman Filter. [Masters Thesis]. Rice University; 2013. Available from: http://hdl.handle.net/1911/71913

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