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You searched for subject:(Guidance Systems Flight ). Showing records 1 – 30 of 63859 total matches.

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East Carolina University

1. Darafsheh, Kaveh. Runtime Monitoring On Hard Real-Time Operating Systems.

Degree: 2015, East Carolina University

 This thesis will compare and evaluate different approaches in integrating runtime monitors into processes running on a hard real-time operating system. The host system is… (more)

Subjects/Keywords: Computer science; Flight control; Guidance systems (Flight); Operating systems (Computers); Computer software

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

APA (6th Edition):

Darafsheh, K. (2015). Runtime Monitoring On Hard Real-Time Operating Systems. (Thesis). East Carolina University. Retrieved from http://hdl.handle.net/10342/4999

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):

Darafsheh, Kaveh. “Runtime Monitoring On Hard Real-Time Operating Systems.” 2015. Thesis, East Carolina University. Accessed December 06, 2019. http://hdl.handle.net/10342/4999.

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

MLA Handbook (7th Edition):

Darafsheh, Kaveh. “Runtime Monitoring On Hard Real-Time Operating Systems.” 2015. Web. 06 Dec 2019.

Vancouver:

Darafsheh K. Runtime Monitoring On Hard Real-Time Operating Systems. [Internet] [Thesis]. East Carolina University; 2015. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10342/4999.

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

Council of Science Editors:

Darafsheh K. Runtime Monitoring On Hard Real-Time Operating Systems. [Thesis]. East Carolina University; 2015. Available from: http://hdl.handle.net/10342/4999

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


University of Arizona

2. Johnson, Morris Ray, 1937-. PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE .

Degree: 1972, University of Arizona

Subjects/Keywords: Guidance systems (Flight); Automatic control.

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APA (6th Edition):

Johnson, Morris Ray, 1. (1972). PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/287885

Chicago Manual of Style (16th Edition):

Johnson, Morris Ray, 1937-. “PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE .” 1972. Doctoral Dissertation, University of Arizona. Accessed December 06, 2019. http://hdl.handle.net/10150/287885.

MLA Handbook (7th Edition):

Johnson, Morris Ray, 1937-. “PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE .” 1972. Web. 06 Dec 2019.

Vancouver:

Johnson, Morris Ray 1. PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE . [Internet] [Doctoral dissertation]. University of Arizona; 1972. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10150/287885.

Council of Science Editors:

Johnson, Morris Ray 1. PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE . [Doctoral Dissertation]. University of Arizona; 1972. Available from: http://hdl.handle.net/10150/287885


Indian Institute of Science

3. Das, Priya G. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.

Degree: 2009, Indian Institute of Science

 To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop”… (more)

Subjects/Keywords: Aerospace Vehicles - Guidance and Control; Interceptors (Aerospace Engineering); Guidance Systems (Flight); Flight Control; Endo-Atmospheric Interceptors; Partial Integrated Guidance and Control; Integrated Guidance and Control (IGC); Impact Angle Constraint; Astronautics

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APA (6th Edition):

Das, P. G. (2009). Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1099

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):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Thesis, Indian Institute of Science. Accessed December 06, 2019. http://hdl.handle.net/2005/1099.

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

MLA Handbook (7th Edition):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Web. 06 Dec 2019.

Vancouver:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2005/1099.

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

Council of Science Editors:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1099

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


Ryerson University

4. Wong, Frank Y.W. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.

Degree: 2009, Ryerson University

 This thesis examines the use of thrusters and solar sails for spacecraft formation keeping control at the Earth-Moon L4 point. Particular emphasis was placed on… (more)

Subjects/Keywords: Space trajectories; Guidance systems (Flight); Navigation (Astronautics); Space vehicles  – Propulsion systems; Space vehicles  – Attitude control systems; Flight control

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APA (6th Edition):

Wong, F. Y. W. (2009). Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Thesis, Ryerson University. Accessed December 06, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

MLA Handbook (7th Edition):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Web. 06 Dec 2019.

Vancouver:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Internet] [Thesis]. Ryerson University; 2009. [cited 2019 Dec 06]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

Council of Science Editors:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Thesis]. Ryerson University; 2009. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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


Georgia Tech

5. Moon, Jongki. Mission-based guidance system design for autonomous UAVs.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The advantages of UAVs in the aviation arena have led to extensive research activities on autonomous technology of UAVs to achieve specific mission objectives. This… (more)

Subjects/Keywords: Obstacle avoidance; Envelope protection; Adptive control; Optimal control; NTG; UAV; Formation flight; Drone aircraft Control systems; Drone aircraft; Guidance systems (Flight)

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

APA (6th Edition):

Moon, J. (2009). Mission-based guidance system design for autonomous UAVs. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/31797

Chicago Manual of Style (16th Edition):

Moon, Jongki. “Mission-based guidance system design for autonomous UAVs.” 2009. Doctoral Dissertation, Georgia Tech. Accessed December 06, 2019. http://hdl.handle.net/1853/31797.

MLA Handbook (7th Edition):

Moon, Jongki. “Mission-based guidance system design for autonomous UAVs.” 2009. Web. 06 Dec 2019.

Vancouver:

Moon J. Mission-based guidance system design for autonomous UAVs. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1853/31797.

Council of Science Editors:

Moon J. Mission-based guidance system design for autonomous UAVs. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/31797


Virginia Tech

6. Katzir, Shevach. Optimal and on-board near-optimal midcourse guidance.

Degree: PhD, Aerospace Engineering, 1988, Virginia Tech

Subjects/Keywords: LD5655.V856 1988.K376; Guided missiles  – Guidance systems; Guidance systems (Flight)

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

APA (6th Edition):

Katzir, S. (1988). Optimal and on-board near-optimal midcourse guidance. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/53546

Chicago Manual of Style (16th Edition):

Katzir, Shevach. “Optimal and on-board near-optimal midcourse guidance.” 1988. Doctoral Dissertation, Virginia Tech. Accessed December 06, 2019. http://hdl.handle.net/10919/53546.

MLA Handbook (7th Edition):

Katzir, Shevach. “Optimal and on-board near-optimal midcourse guidance.” 1988. Web. 06 Dec 2019.

Vancouver:

Katzir S. Optimal and on-board near-optimal midcourse guidance. [Internet] [Doctoral dissertation]. Virginia Tech; 1988. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10919/53546.

Council of Science Editors:

Katzir S. Optimal and on-board near-optimal midcourse guidance. [Doctoral Dissertation]. Virginia Tech; 1988. Available from: http://hdl.handle.net/10919/53546


Virginia Tech

7. Hartman, Richard Donald. Optimal maneuver guidance with sensor line of sight constraint.

Degree: PhD, Aerospace and Ocean Engineering, 1992, Virginia Tech

 The problem of optimal guidance design for the low altitude, subsonic, vertical plane approach maneuver of an air vehicle constrained to maintain view of a… (more)

Subjects/Keywords: Guidance systems (Flight) Mathematical models.; LD5655.V856 1992.H377

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APA (6th Edition):

Hartman, R. D. (1992). Optimal maneuver guidance with sensor line of sight constraint. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/39435

Chicago Manual of Style (16th Edition):

Hartman, Richard Donald. “Optimal maneuver guidance with sensor line of sight constraint.” 1992. Doctoral Dissertation, Virginia Tech. Accessed December 06, 2019. http://hdl.handle.net/10919/39435.

MLA Handbook (7th Edition):

Hartman, Richard Donald. “Optimal maneuver guidance with sensor line of sight constraint.” 1992. Web. 06 Dec 2019.

Vancouver:

Hartman RD. Optimal maneuver guidance with sensor line of sight constraint. [Internet] [Doctoral dissertation]. Virginia Tech; 1992. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10919/39435.

Council of Science Editors:

Hartman RD. Optimal maneuver guidance with sensor line of sight constraint. [Doctoral Dissertation]. Virginia Tech; 1992. Available from: http://hdl.handle.net/10919/39435


Virginia Tech

8. Bushong, Philip Merton. A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously.

Degree: PhD, Aerospace Engineering, 1991, Virginia Tech

 A design method for a multi-loop mixed discrete/continuous trajectory following pitch control algorithm for a generic aerospace vehicle is presented. This design methodology is facilitated… (more)

Subjects/Keywords: Guidance systems (Flight); LD5655.V856 1991.B885

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APA (6th Edition):

Bushong, P. M. (1991). A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/38982

Chicago Manual of Style (16th Edition):

Bushong, Philip Merton. “A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously.” 1991. Doctoral Dissertation, Virginia Tech. Accessed December 06, 2019. http://hdl.handle.net/10919/38982.

MLA Handbook (7th Edition):

Bushong, Philip Merton. “A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously.” 1991. Web. 06 Dec 2019.

Vancouver:

Bushong PM. A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously. [Internet] [Doctoral dissertation]. Virginia Tech; 1991. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10919/38982.

Council of Science Editors:

Bushong PM. A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously. [Doctoral Dissertation]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/38982


University of Adelaide

9. Hassoun, George Estandy. A study of observability-enhanced guidance systems / by George Estandy Hassoun.

Degree: 1995, University of Adelaide

 This thesis investigates a novel guidance law dubbed "observable proportional navigation". Two distinct forms of this guidance law are considered, based on the nature of… (more)

Subjects/Keywords: Guidance systems (Flight); Observers (Control theory); Proportional navigation.

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APA (6th Edition):

Hassoun, G. E. (1995). A study of observability-enhanced guidance systems / by George Estandy Hassoun. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/18618

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):

Hassoun, George Estandy. “A study of observability-enhanced guidance systems / by George Estandy Hassoun.” 1995. Thesis, University of Adelaide. Accessed December 06, 2019. http://hdl.handle.net/2440/18618.

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

MLA Handbook (7th Edition):

Hassoun, George Estandy. “A study of observability-enhanced guidance systems / by George Estandy Hassoun.” 1995. Web. 06 Dec 2019.

Vancouver:

Hassoun GE. A study of observability-enhanced guidance systems / by George Estandy Hassoun. [Internet] [Thesis]. University of Adelaide; 1995. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2440/18618.

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

Council of Science Editors:

Hassoun GE. A study of observability-enhanced guidance systems / by George Estandy Hassoun. [Thesis]. University of Adelaide; 1995. Available from: http://hdl.handle.net/2440/18618

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


Drexel University

10. Ilg, Mark Dean. Guidance, navigation, and control for munitions.

Degree: 2008, Drexel University

The United States Army is currently looking for new methods of guiding munitions, which would allow the military to employ guided munitions in place of… (more)

Subjects/Keywords: Mechanical engineering; Military weapons; Guidance systems (Flight)

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APA (6th Edition):

Ilg, M. D. (2008). Guidance, navigation, and control for munitions. (Thesis). Drexel University. Retrieved from http://hdl.handle.net/1860/2831

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):

Ilg, Mark Dean. “Guidance, navigation, and control for munitions.” 2008. Thesis, Drexel University. Accessed December 06, 2019. http://hdl.handle.net/1860/2831.

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

MLA Handbook (7th Edition):

Ilg, Mark Dean. “Guidance, navigation, and control for munitions.” 2008. Web. 06 Dec 2019.

Vancouver:

Ilg MD. Guidance, navigation, and control for munitions. [Internet] [Thesis]. Drexel University; 2008. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1860/2831.

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

Council of Science Editors:

Ilg MD. Guidance, navigation, and control for munitions. [Thesis]. Drexel University; 2008. Available from: http://hdl.handle.net/1860/2831

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


Stellenbosch University

11. Bijker, Johan. Development of an attitude heading reference system for an airship.

Degree: Electrical and Electronic Engineering, 2006, Stellenbosch University

Thesis (MScEng (Electrical and Electronic Engineering)) – University of Stellenbosch, 2006.

A real time attitude and heading reference system (AHRS) was successfully implemented for use on… (more)

Subjects/Keywords: Electronic engineering; Dissertations  – Electronic engineering; Airships; Flight control; Guidance systems (Flight); Drone aircraft

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APA (6th Edition):

Bijker, J. (2006). Development of an attitude heading reference system for an airship. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/1551

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):

Bijker, Johan. “Development of an attitude heading reference system for an airship.” 2006. Thesis, Stellenbosch University. Accessed December 06, 2019. http://hdl.handle.net/10019.1/1551.

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

MLA Handbook (7th Edition):

Bijker, Johan. “Development of an attitude heading reference system for an airship.” 2006. Web. 06 Dec 2019.

Vancouver:

Bijker J. Development of an attitude heading reference system for an airship. [Internet] [Thesis]. Stellenbosch University; 2006. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10019.1/1551.

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

Council of Science Editors:

Bijker J. Development of an attitude heading reference system for an airship. [Thesis]. Stellenbosch University; 2006. Available from: http://hdl.handle.net/10019.1/1551

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


Virginia Tech

12. Visser, Hendrikus. Energy management of three-dimensional minimum-time intercept.

Degree: PhD, Aerospace and Ocean Engineering, 1985, Virginia Tech

Subjects/Keywords: LD5655.V856 1985.V567; Trajectory optimization; Guidance systems (Flight); Singular perturbations (Mathematics)

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APA (6th Edition):

Visser, H. (1985). Energy management of three-dimensional minimum-time intercept. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49954

Chicago Manual of Style (16th Edition):

Visser, Hendrikus. “Energy management of three-dimensional minimum-time intercept.” 1985. Doctoral Dissertation, Virginia Tech. Accessed December 06, 2019. http://hdl.handle.net/10919/49954.

MLA Handbook (7th Edition):

Visser, Hendrikus. “Energy management of three-dimensional minimum-time intercept.” 1985. Web. 06 Dec 2019.

Vancouver:

Visser H. Energy management of three-dimensional minimum-time intercept. [Internet] [Doctoral dissertation]. Virginia Tech; 1985. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/10919/49954.

Council of Science Editors:

Visser H. Energy management of three-dimensional minimum-time intercept. [Doctoral Dissertation]. Virginia Tech; 1985. Available from: http://hdl.handle.net/10919/49954


Cal Poly

13. Fujizawa, Brian T. Control Law Design and Validation for a Helicopter In-Flight Simulator.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 In-flight simulation allows one aircraft to simulate the dynamic response of another aircraft. A control system designed to give RASCAL, a JUH-60A Black Hawk helicopter… (more)

Subjects/Keywords: Helicopter; In-flight simulation; flight controls; simulation; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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

APA (6th Edition):

Fujizawa, B. T. (2010). Control Law Design and Validation for a Helicopter In-Flight Simulator. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10

Chicago Manual of Style (16th Edition):

Fujizawa, Brian T. “Control Law Design and Validation for a Helicopter In-Flight Simulator.” 2010. Masters Thesis, Cal Poly. Accessed December 06, 2019. https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10.

MLA Handbook (7th Edition):

Fujizawa, Brian T. “Control Law Design and Validation for a Helicopter In-Flight Simulator.” 2010. Web. 06 Dec 2019.

Vancouver:

Fujizawa BT. Control Law Design and Validation for a Helicopter In-Flight Simulator. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10.

Council of Science Editors:

Fujizawa BT. Control Law Design and Validation for a Helicopter In-Flight Simulator. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10


Georgia Tech

14. Sattigeri, Ramachandra Jayant. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

 The role of vision as an additional sensing mechanism has received a lot of attention in recent years in the context of autonomous flight applications.… (more)

Subjects/Keywords: Neural networks; Target tracking; Adaptive estimation; Adaptive Kalman filters; Integrated guidance and control; Adaptive guidance and control; Adaptive control; Unmanned aerial vehicles; Multiple-vehicle formation; Guidance systems (Flight); Robot vision; Adaptive control systems; Drone aircraft; Flight control

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

APA (6th Edition):

Sattigeri, R. J. (2007). Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/16272

Chicago Manual of Style (16th Edition):

Sattigeri, Ramachandra Jayant. “Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.” 2007. Doctoral Dissertation, Georgia Tech. Accessed December 06, 2019. http://hdl.handle.net/1853/16272.

MLA Handbook (7th Edition):

Sattigeri, Ramachandra Jayant. “Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.” 2007. Web. 06 Dec 2019.

Vancouver:

Sattigeri RJ. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1853/16272.

Council of Science Editors:

Sattigeri RJ. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. [Doctoral Dissertation]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/16272


Indian Institute of Science

15. Saroj Kumar, G. An Integrated Estimation-Guidance Approach for Seeker-less Interceptors.

Degree: 2015, Indian Institute of Science

 In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less interceptors that operate in the command guidance mode, is addressed. These systems are… (more)

Subjects/Keywords: Guided Missiles; Planar Interception; Seeker-less Interceptors; Kalman Filters; Interactive Multiple Model; Fighter Aircraft Interception; Helicopter Interception; Missile Guided Systems; Guided Systems(Flight); Guided Missiles-Control Systems; Guidance Laws; Seeker-less Interceptor; Aerospace Engineering

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APA (6th Edition):

Saroj Kumar, G. (2015). An Integrated Estimation-Guidance Approach for Seeker-less Interceptors. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3828 ; http://etd.iisc.ernet.in/abstracts/4700/G26981-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):

Saroj Kumar, G. “An Integrated Estimation-Guidance Approach for Seeker-less Interceptors.” 2015. Thesis, Indian Institute of Science. Accessed December 06, 2019. http://etd.iisc.ernet.in/2005/3828 ; http://etd.iisc.ernet.in/abstracts/4700/G26981-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):

Saroj Kumar, G. “An Integrated Estimation-Guidance Approach for Seeker-less Interceptors.” 2015. Web. 06 Dec 2019.

Vancouver:

Saroj Kumar G. An Integrated Estimation-Guidance Approach for Seeker-less Interceptors. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 06]. Available from: http://etd.iisc.ernet.in/2005/3828 ; http://etd.iisc.ernet.in/abstracts/4700/G26981-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:

Saroj Kumar G. An Integrated Estimation-Guidance Approach for Seeker-less Interceptors. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3828 ; http://etd.iisc.ernet.in/abstracts/4700/G26981-Abs.pdf

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


Indian Institute of Science

16. Kumar, Shashi Ranjan. Sliding Mode Control Based Guidance Strategies with Terminal Constraints.

Degree: 2015, Indian Institute of Science

 In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional… (more)

Subjects/Keywords: Sliding Mode Control; Guidance and Control Theory; Sliding Mode Guidance Laws; Impact Angle Guidance; Impact Time Guidance; Guidance Laws; Sliding Mode Guidance; Salvo Attack Guidance; Nonlinear Engagement Dynamics; Missile Guidance; Flight Control; Finite Time Convergence; Sliding-Mode Guidance; Impact Time Guidance; Aerospace Engineering

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APA (6th Edition):

Kumar, S. R. (2015). Sliding Mode Control Based Guidance Strategies with Terminal Constraints. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-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):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Thesis, Indian Institute of Science. Accessed December 06, 2019. http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-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):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Web. 06 Dec 2019.

Vancouver:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 06]. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-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:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf

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


University of Toronto

17. Newman, Josh Zachary. Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission.

Degree: 2015, University of Toronto

Canadian Advanced Nanospace eXperiments 4 5 (CanX-45) are a pair of formation flying nanosatellites that demonstrated autonomous sub-metre formation control at ranges of 1000 to… (more)

Subjects/Keywords: Control; Formation Flight; Guidance; Microsatellite; Nanosatellite; Navigation; 0538

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APA (6th Edition):

Newman, J. Z. (2015). Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/69688

Chicago Manual of Style (16th Edition):

Newman, Josh Zachary. “Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission.” 2015. Masters Thesis, University of Toronto. Accessed December 06, 2019. http://hdl.handle.net/1807/69688.

MLA Handbook (7th Edition):

Newman, Josh Zachary. “Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission.” 2015. Web. 06 Dec 2019.

Vancouver:

Newman JZ. Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission. [Internet] [Masters thesis]. University of Toronto; 2015. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1807/69688.

Council of Science Editors:

Newman JZ. Drift Recovery and Station Keeping for the CANX-4 and CANX-5 Nanosatellite Formation Flying Mission. [Masters Thesis]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69688

18. Rogers, Jonathan. Applications of internal translating mass technologies to smart weapons systems.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The field of guided projectile research has continually grown over the past several decades. Guided projectiles, typically encompassing bullets, mortars, and artillery shells, incorporate some… (more)

Subjects/Keywords: Internal translating mass; Moving mass; Flight control; Missiles; Projectiles; Smart weapons; Machine translating; Precision guided munitions; Guidance systems (Flight); Guided missiles Guidance systems

…Hybrid SMC 152 6.3.4 Flight Control System Test Case 156 6.3.5 Sliding Mode Control of an… …Percentages. 111 Table 5.1: Munition Launch and Flight Survivability Requirements. 117 Table 5.2… …Flight. 120 Figure 5.2: Projectile with Sensor Suite Shock Absorber. 121 Figure 5.3… …Guided Munition PNG Proportional Navigation Guidance PRIM Partially-Restrained Internal… …incorporate some sort of guidance and control mechanism to generate trajectory alterations. This… 

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APA (6th Edition):

Rogers, J. (2009). Applications of internal translating mass technologies to smart weapons systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/31813

Chicago Manual of Style (16th Edition):

Rogers, Jonathan. “Applications of internal translating mass technologies to smart weapons systems.” 2009. Doctoral Dissertation, Georgia Tech. Accessed December 06, 2019. http://hdl.handle.net/1853/31813.

MLA Handbook (7th Edition):

Rogers, Jonathan. “Applications of internal translating mass technologies to smart weapons systems.” 2009. Web. 06 Dec 2019.

Vancouver:

Rogers J. Applications of internal translating mass technologies to smart weapons systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1853/31813.

Council of Science Editors:

Rogers J. Applications of internal translating mass technologies to smart weapons systems. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/31813


Cape Peninsula University of Technology

19. Petersen, Michael. Development of a seamless morphing wing .

Degree: 2010, Cape Peninsula University of Technology

 The Cape Peninsula University of Technology (CPUT) Advanced Manufacturing and Technology Laboratory (AMTL) developed an Unmanned Aerial Vehicle (UAV) Technology Demonstrator for the purpose of… (more)

Subjects/Keywords: Morphing; Drone aircraft  – Control systems; Flight simulators; Flight control

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APA (6th Edition):

Petersen, M. (2010). Development of a seamless morphing wing . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/2230

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):

Petersen, Michael. “Development of a seamless morphing wing .” 2010. Thesis, Cape Peninsula University of Technology. Accessed December 06, 2019. http://etd.cput.ac.za/handle/20.500.11838/2230.

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

MLA Handbook (7th Edition):

Petersen, Michael. “Development of a seamless morphing wing .” 2010. Web. 06 Dec 2019.

Vancouver:

Petersen M. Development of a seamless morphing wing . [Internet] [Thesis]. Cape Peninsula University of Technology; 2010. [cited 2019 Dec 06]. Available from: http://etd.cput.ac.za/handle/20.500.11838/2230.

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

Council of Science Editors:

Petersen M. Development of a seamless morphing wing . [Thesis]. Cape Peninsula University of Technology; 2010. Available from: http://etd.cput.ac.za/handle/20.500.11838/2230

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

20. Kang, Keeryun. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis presents an integrated framework for online obstacle avoidance of rotary-wing unmanned aerial vehicles (UAVs), which can provide UAVs an obstacle field navigation capability… (more)

Subjects/Keywords: Real-time optimization; Trajectory optimization; UAV; Obstacle avoidance; Trajectory planning; Guidance systems (Flight); Drone aircraft; Flight control

…viii LIST OF TABLES 1 Limit values for the flight test… …INTOPTOA to baseline time to maneuver 5 Summary of INTOPTOA flight test results 6 Yamaha Rmax… …arbitrary multiple manifolds . . . . . . . 66 19 Software implementation for the first flight… …test . . . . . . . . . . . . 67 20 Time-optimal flight test cases and avoidance conditions… …68 21 Time-optimal flight test case0 . . . . . . . . . . . . . . . . . . . . . . 69 22… 

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APA (6th Edition):

Kang, K. (2012). Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44820

Chicago Manual of Style (16th Edition):

Kang, Keeryun. “Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.” 2012. Doctoral Dissertation, Georgia Tech. Accessed December 06, 2019. http://hdl.handle.net/1853/44820.

MLA Handbook (7th Edition):

Kang, Keeryun. “Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.” 2012. Web. 06 Dec 2019.

Vancouver:

Kang K. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1853/44820.

Council of Science Editors:

Kang K. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44820

21. Lopez, Christian W. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  The control of multiple unmanned aerial vehicles (UAVs) in a swarm or cooperative team scenario has been a topic of great interest for well… (more)

Subjects/Keywords: UAV; Formation Flight; Simulation; Flight Testing; Multi-Vehicle Systems and Air Traffic Control; Navigation, Guidance, Control and Dynamics

…simulation and the small embedded control systems used in flight. These computational limitations… …of full implementation and flight test evaluation using embedded control systems. This lack… …function guidance, as well as simulation and flight testing for small UAVs. A brief review of… …flight capability in this work. This guidance method has been a common thread in the previous… …Awareness . . . . . . . . . . . . . . 16 2.9 Potential Function Guidance… 

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APA (6th Edition):

Lopez, C. W. (2013). UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103

Chicago Manual of Style (16th Edition):

Lopez, Christian W. “UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.” 2013. Masters Thesis, Cal Poly. Accessed December 06, 2019. https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103.

MLA Handbook (7th Edition):

Lopez, Christian W. “UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.” 2013. Web. 06 Dec 2019.

Vancouver:

Lopez CW. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103.

Council of Science Editors:

Lopez CW. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103

22. Abdallah, Ayman Muhammad. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.

Degree: PhD, Aerospace Engineering, 2015, Old Dominion University

  A new asymmetric level aerodynamic attitude flight envelope is introduced in this dissertation. The aerodynamic attitude envelope is an angle of attack vs. sideslip… (more)

Subjects/Keywords: Aerodynamic attitude flight envelope; Airplanes; Speed; Flight dynamics; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Abdallah, A. M. (2015). Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107

Chicago Manual of Style (16th Edition):

Abdallah, Ayman Muhammad. “Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.” 2015. Doctoral Dissertation, Old Dominion University. Accessed December 06, 2019. 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107.

MLA Handbook (7th Edition):

Abdallah, Ayman Muhammad. “Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.” 2015. Web. 06 Dec 2019.

Vancouver:

Abdallah AM. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. [Internet] [Doctoral dissertation]. Old Dominion University; 2015. [cited 2019 Dec 06]. Available from: 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107.

Council of Science Editors:

Abdallah AM. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. [Doctoral Dissertation]. Old Dominion University; 2015. Available from: 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107


KTH

23. Knöös, Johan. Control of a Reusable Launch Vehicle.

Degree: Mathematics (Dept.), 2011, KTH

  Abstrakt: This report examines different control design methods, linear as well as nonlinear, for a suborbital reusable launch vehicle. An investigation of the natural… (more)

Subjects/Keywords: Flight control systems; nonlinear control; global optimization

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APA (6th Edition):

Knöös, J. (2011). Control of a Reusable Launch Vehicle. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837

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):

Knöös, Johan. “Control of a Reusable Launch Vehicle.” 2011. Thesis, KTH. Accessed December 06, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837.

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

MLA Handbook (7th Edition):

Knöös, Johan. “Control of a Reusable Launch Vehicle.” 2011. Web. 06 Dec 2019.

Vancouver:

Knöös J. Control of a Reusable Launch Vehicle. [Internet] [Thesis]. KTH; 2011. [cited 2019 Dec 06]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837.

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

Council of Science Editors:

Knöös J. Control of a Reusable Launch Vehicle. [Thesis]. KTH; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837

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


Ryerson University

24. Li, Junquan. Intelligent Control of Satellite Formation Flying.

Degree: 2012, Ryerson University

 Small satellites flying in formation present a more efficient and affordable way of achieving the same or better performance than a large satellite because of… (more)

Subjects/Keywords: Space dynamics; Space vehicles  – Control systems; Space flight; Flight control; Artificial satellites  – Control systems

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APA (6th Edition):

Li, J. (2012). Intelligent Control of Satellite Formation Flying. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A2347

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):

Li, Junquan. “Intelligent Control of Satellite Formation Flying.” 2012. Thesis, Ryerson University. Accessed December 06, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A2347.

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

MLA Handbook (7th Edition):

Li, Junquan. “Intelligent Control of Satellite Formation Flying.” 2012. Web. 06 Dec 2019.

Vancouver:

Li J. Intelligent Control of Satellite Formation Flying. [Internet] [Thesis]. Ryerson University; 2012. [cited 2019 Dec 06]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2347.

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

Council of Science Editors:

Li J. Intelligent Control of Satellite Formation Flying. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2347

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


Texas A&M University

25. Wirthman, David James. A parallel implementation of the parallel-shooting method for trajectory optimization.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Trajectory optimization.; Guidance systems (Flight); Vertically rising aircraft - Aerodynamics.; Parallel processing (Electronic computers)

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APA (6th Edition):

Wirthman, D. J. (2012). A parallel implementation of the parallel-shooting method for trajectory optimization. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-W799

Chicago Manual of Style (16th Edition):

Wirthman, David James. “A parallel implementation of the parallel-shooting method for trajectory optimization.” 2012. Masters Thesis, Texas A&M University. Accessed December 06, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-W799.

MLA Handbook (7th Edition):

Wirthman, David James. “A parallel implementation of the parallel-shooting method for trajectory optimization.” 2012. Web. 06 Dec 2019.

Vancouver:

Wirthman DJ. A parallel implementation of the parallel-shooting method for trajectory optimization. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-W799.

Council of Science Editors:

Wirthman DJ. A parallel implementation of the parallel-shooting method for trajectory optimization. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-W799

26. Al-Shenhabi, Abdul Ghafoor. Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications.

Degree: PhD, Aerospace Engineering, 2001, Old Dominion University

  An important step in control design for elastic systems is the determination of the number and location of control system components, namely sensors. The… (more)

Subjects/Keywords: Aeroelastic; Flight control; Root migration; Vehicle sensor; Navigation, Guidance, Control and Dynamics; Structures and Materials; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Al-Shenhabi, A. G. (2001). Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780493564951 ; https://digitalcommons.odu.edu/mae_etds/50

Chicago Manual of Style (16th Edition):

Al-Shenhabi, Abdul Ghafoor. “Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications.” 2001. Doctoral Dissertation, Old Dominion University. Accessed December 06, 2019. 9780493564951 ; https://digitalcommons.odu.edu/mae_etds/50.

MLA Handbook (7th Edition):

Al-Shenhabi, Abdul Ghafoor. “Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications.” 2001. Web. 06 Dec 2019.

Vancouver:

Al-Shenhabi AG. Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications. [Internet] [Doctoral dissertation]. Old Dominion University; 2001. [cited 2019 Dec 06]. Available from: 9780493564951 ; https://digitalcommons.odu.edu/mae_etds/50.

Council of Science Editors:

Al-Shenhabi AG. Optimal Aeroelastic Vehicle Sensor Placement for Root Migration Flight Control Applications. [Doctoral Dissertation]. Old Dominion University; 2001. Available from: 9780493564951 ; https://digitalcommons.odu.edu/mae_etds/50


Université de Lorraine

27. Sève, Florian. Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles.

Degree: Docteur es, Automatique, Traitement du Signal et des Images, Génie Informatique, 2016, Université de Lorraine

Ce mémoire de thèse traite du développement des dynamiques et des lois de commande de vol d’un projectile d’artillerie gyrostabilisé guidé par une tête découplée.… (more)

Subjects/Keywords: Projectiles guidés; Mécanique du vol; Systèmes dynamiques non linéaires, q-LPV et incertains; Commande robuste H∞; Séquencement de gains; Guidage par navigation proportionnelle; Guided projectiles; Flight mechanics; Nonlinear, q-LPV and uncertain dynamic systems; H∞ robust control; Gain-Scheduling; Proportional navigation guidance; 629.8

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APA (6th Edition):

Sève, F. (2016). Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles. (Doctoral Dissertation). Université de Lorraine. Retrieved from http://www.theses.fr/2016LORR0281

Chicago Manual of Style (16th Edition):

Sève, Florian. “Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles.” 2016. Doctoral Dissertation, Université de Lorraine. Accessed December 06, 2019. http://www.theses.fr/2016LORR0281.

MLA Handbook (7th Edition):

Sève, Florian. “Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles.” 2016. Web. 06 Dec 2019.

Vancouver:

Sève F. Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles. [Internet] [Doctoral dissertation]. Université de Lorraine; 2016. [cited 2019 Dec 06]. Available from: http://www.theses.fr/2016LORR0281.

Council of Science Editors:

Sève F. Commande robuste pour une classe de systèmes non linéaires à paramètres variants : application aux projectiles guidés : Robust Control for a Class of Nonlinear Parameter-Varying Systems : Application to Guided Projectiles. [Doctoral Dissertation]. Université de Lorraine; 2016. Available from: http://www.theses.fr/2016LORR0281


Purdue University

28. Kane, Anthony Mark. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).

Degree: MS, Aeronautics and Astronautics, 2014, Purdue University

  An integrated software architecture for development of unmanned research vehicles is developed. It has been created under the premise that all unmanned vehicles require… (more)

Subjects/Keywords: Applied sciences; Control; Guidance; Integrated flight software; Navigation; Aerospace Engineering; Computer Engineering

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APA (6th Edition):

Kane, A. M. (2014). Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/338

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):

Kane, Anthony Mark. “Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).” 2014. Thesis, Purdue University. Accessed December 06, 2019. http://docs.lib.purdue.edu/open_access_theses/338.

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

MLA Handbook (7th Edition):

Kane, Anthony Mark. “Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).” 2014. Web. 06 Dec 2019.

Vancouver:

Kane AM. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). [Internet] [Thesis]. Purdue University; 2014. [cited 2019 Dec 06]. Available from: http://docs.lib.purdue.edu/open_access_theses/338.

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

Council of Science Editors:

Kane AM. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). [Thesis]. Purdue University; 2014. Available from: http://docs.lib.purdue.edu/open_access_theses/338

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

29. Tran, Thanh Trung. Nonlinear Flight Control Design Using Backstepping Methodology.

Degree: PhD, Aerospace Engineering, 2016, Old Dominion University

  The subject of nonlinear flight control design using backstepping control methodology is investigated in the dissertation research presented here. Control design methods based on… (more)

Subjects/Keywords: Backstepping control; Lyapunov-Based Design; Nonlinear flight control; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Tran, T. T. (2016). Nonlinear Flight Control Design Using Backstepping Methodology. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16

Chicago Manual of Style (16th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Doctoral Dissertation, Old Dominion University. Accessed December 06, 2019. 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

MLA Handbook (7th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Web. 06 Dec 2019.

Vancouver:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Internet] [Doctoral dissertation]. Old Dominion University; 2016. [cited 2019 Dec 06]. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

Council of Science Editors:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Doctoral Dissertation]. Old Dominion University; 2016. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16


Univerzitet u Beogradu

30. Marković, Miloš Д., 1987-. Синтеза тактичких ракета земља-ваздух против циљева великих брзина.

Degree: Mašinski fakultet, 2018, Univerzitet u Beogradu

Машинство-Војно машинство-Системи наоружања, ракетни системи / Mechanical engineering Scientific subdiscipline: Military engineering - Weapon systems, Missile systems

У раду је представљен интегрални приступ истраживању параметара… (more)

Subjects/Keywords: missile design; aerodynamics; guidance and control; explosively formed projectile; nonlinear simulation; propulsion; flight dynamics

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

APA (6th Edition):

Marković, Miloš Д., 1. (2018). Синтеза тактичких ракета земља-ваздух против циљева великих брзина. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/get

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):

Marković, Miloš Д., 1987-. “Синтеза тактичких ракета земља-ваздух против циљева великих брзина.” 2018. Thesis, Univerzitet u Beogradu. Accessed December 06, 2019. https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/get.

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

MLA Handbook (7th Edition):

Marković, Miloš Д., 1987-. “Синтеза тактичких ракета земља-ваздух против циљева великих брзина.” 2018. Web. 06 Dec 2019.

Vancouver:

Marković, Miloš Д. 1. Синтеза тактичких ракета земља-ваздух против циљева великих брзина. [Internet] [Thesis]. Univerzitet u Beogradu; 2018. [cited 2019 Dec 06]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/get.

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

Council of Science Editors:

Marković, Miloš Д. 1. Синтеза тактичких ракета земља-ваздух против циљева великих брзина. [Thesis]. Univerzitet u Beogradu; 2018. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/get

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

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