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You searched for subject:(Proportional Navigation). Showing records 1 – 14 of 14 total matches.

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Texas A&M University

1. Kim, Byungjun. Proportional-Integral-Derivative Controller in Proportional Navigation Guidance.

Degree: MS, Electrical Engineering, 2016, Texas A&M University

 In this thesis, a Proportional-Integral-Derivative (PID) guidance scheme is discussed to improve the miss distance accuracy and the finite time stability problem in the Proportional(more)

Subjects/Keywords: PID guidance; Proportional Navigation Guidance

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APA (6th Edition):

Kim, B. (2016). Proportional-Integral-Derivative Controller in Proportional Navigation Guidance. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157866

Chicago Manual of Style (16th Edition):

Kim, Byungjun. “Proportional-Integral-Derivative Controller in Proportional Navigation Guidance.” 2016. Masters Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/157866.

MLA Handbook (7th Edition):

Kim, Byungjun. “Proportional-Integral-Derivative Controller in Proportional Navigation Guidance.” 2016. Web. 08 Dec 2019.

Vancouver:

Kim B. Proportional-Integral-Derivative Controller in Proportional Navigation Guidance. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/157866.

Council of Science Editors:

Kim B. Proportional-Integral-Derivative Controller in Proportional Navigation Guidance. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/157866


University of Arizona

2. Cottrell, Ronald Gelnn, 1942-. Optimal and suboptimal corrections for proportional navigation .

Degree: 1970, University of Arizona

Subjects/Keywords: Guided missiles  – Guidance systems.; Proportional navigation.

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APA (6th Edition):

Cottrell, Ronald Gelnn, 1. (1970). Optimal and suboptimal corrections for proportional navigation . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/318092

Chicago Manual of Style (16th Edition):

Cottrell, Ronald Gelnn, 1942-. “Optimal and suboptimal corrections for proportional navigation .” 1970. Masters Thesis, University of Arizona. Accessed December 08, 2019. http://hdl.handle.net/10150/318092.

MLA Handbook (7th Edition):

Cottrell, Ronald Gelnn, 1942-. “Optimal and suboptimal corrections for proportional navigation .” 1970. Web. 08 Dec 2019.

Vancouver:

Cottrell, Ronald Gelnn 1. Optimal and suboptimal corrections for proportional navigation . [Internet] [Masters thesis]. University of Arizona; 1970. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/10150/318092.

Council of Science Editors:

Cottrell, Ronald Gelnn 1. Optimal and suboptimal corrections for proportional navigation . [Masters Thesis]. University of Arizona; 1970. Available from: http://hdl.handle.net/10150/318092


Indian Institute of Science

3. Ghosh, Satadal. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.

Degree: 2014, Indian Institute of Science

 Guidance is defined as the determination of a strategy for following a nominal path in the presence of o-nominal conditions, disturbances and uncertainties, and the… (more)

Subjects/Keywords: Proportional Navigation; Maneuvering Target; Guidance; Augumented Pure Portional Navigation (APPN) Guidance Laws; Retro-PN Guidance Law; Guidance Laws; Higher-Speed Target; Agile Targets; Impact Angle Control; Composite Proportional Navigation (CPN); Impact Angle Analysis; Impact Time Control; Salvo Attack; Higher Speed Nonmaneuvering Targets; Time-varying Target; Mathematics

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APA (6th Edition):

Ghosh, S. (2014). Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2903

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):

Ghosh, Satadal. “Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.” 2014. Thesis, Indian Institute of Science. Accessed December 08, 2019. http://hdl.handle.net/2005/2903.

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

MLA Handbook (7th Edition):

Ghosh, Satadal. “Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.” 2014. Web. 08 Dec 2019.

Vancouver:

Ghosh S. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2005/2903.

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

Council of Science Editors:

Ghosh S. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/2903

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


KTH

4. Sefastsson, Ulf. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.

Degree: Optimization and Systems Theory, 2016, KTH

Missile guidance and autopilot have been active fields of research since the second world war. There are lots of literature on the subjects, but… (more)

Subjects/Keywords: Missile Guidance; Proportional Navigation; Optimal Guidance; Differential Game Guidance; Model Predictive Control.; Missilstyrning; syftbäringsstyrning; optimal missilstyrning; spelteoretisk missilstyrning; modellprediktiv reglering

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APA (6th Edition):

Sefastsson, U. (2016). Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897

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):

Sefastsson, Ulf. “Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.” 2016. Thesis, KTH. Accessed December 08, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897.

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

MLA Handbook (7th Edition):

Sefastsson, Ulf. “Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.” 2016. Web. 08 Dec 2019.

Vancouver:

Sefastsson U. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. [Internet] [Thesis]. KTH; 2016. [cited 2019 Dec 08]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897.

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

Council of Science Editors:

Sefastsson U. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. [Thesis]. KTH; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897

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


University of Adelaide

5. 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 08, 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. 08 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 08]. 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


Linköping University

6. Persson, Mathias. Optimering av slutfasstyrning.

Degree: Electrical Engineering, 2002, Linköping University

  Modern missiles must meet higher and higher demands. They should be autonomous, have long range and still have a big effect on the target.… (more)

Subjects/Keywords: Reglerteknik; slutfasstyrning; optimering; proportional navigation; referensbana; bangenerering; missilstyrning; reglerteknik; Reglerteknik; Automatic control; Reglerteknik

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APA (6th Edition):

Persson, M. (2002). Optimering av slutfasstyrning. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1416

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):

Persson, Mathias. “Optimering av slutfasstyrning.” 2002. Thesis, Linköping University. Accessed December 08, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1416.

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

MLA Handbook (7th Edition):

Persson, Mathias. “Optimering av slutfasstyrning.” 2002. Web. 08 Dec 2019.

Vancouver:

Persson M. Optimering av slutfasstyrning. [Internet] [Thesis]. Linköping University; 2002. [cited 2019 Dec 08]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1416.

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

Council of Science Editors:

Persson M. Optimering av slutfasstyrning. [Thesis]. Linköping University; 2002. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1416

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


University of Arizona

7. Morgan, Robert W. A New Paradigm in Optimal Missile Guidance .

Degree: 2007, University of Arizona

 This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of missile guidance usually lasts less than ten seconds and calls for very… (more)

Subjects/Keywords: missile guidance; Lyapunov; optimal control; proportional navigation; optimal guidance; optimal control

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APA (6th Edition):

Morgan, R. W. (2007). A New Paradigm in Optimal Missile Guidance . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/194121

Chicago Manual of Style (16th Edition):

Morgan, Robert W. “A New Paradigm in Optimal Missile Guidance .” 2007. Doctoral Dissertation, University of Arizona. Accessed December 08, 2019. http://hdl.handle.net/10150/194121.

MLA Handbook (7th Edition):

Morgan, Robert W. “A New Paradigm in Optimal Missile Guidance .” 2007. Web. 08 Dec 2019.

Vancouver:

Morgan RW. A New Paradigm in Optimal Missile Guidance . [Internet] [Doctoral dissertation]. University of Arizona; 2007. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/10150/194121.

Council of Science Editors:

Morgan RW. A New Paradigm in Optimal Missile Guidance . [Doctoral Dissertation]. University of Arizona; 2007. Available from: http://hdl.handle.net/10150/194121


Université de Lorraine

8. 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 08, 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. 08 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 08]. 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

9. Tan, Ruoyu. Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles.

Degree: MS, Engineering and Applied Science: Mechanical Engineering, 2013, University of Cincinnati

 An Unmanned Air Vehicle (UAV) is an aircraft without a human pilot on board. It can be controlled either autonomously by computers onboard, or using… (more)

Subjects/Keywords: Mechanical Engineering; Unmanned Air Vehicle; quadrotor UAV; multicopter; Proportional Navigation; Trajectory Generation

Proportional Navigation (PN) based tracking strategy to solve the first problem presented… …Proportional Navigation method is found to its accommodate for our quadrotor dynamics better than… …tracking result. Subsequently, features and research progress of existing Proportional Navigation… …layer in [15] . 2.3 Existing Tracking Methods Proportional navigation (PN… …addition, a proportional navigation guidance based technique [23] has been used for… 

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APA (6th Edition):

Tan, R. (2013). Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378194694

Chicago Manual of Style (16th Edition):

Tan, Ruoyu. “Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles.” 2013. Masters Thesis, University of Cincinnati. Accessed December 08, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378194694.

MLA Handbook (7th Edition):

Tan, Ruoyu. “Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles.” 2013. Web. 08 Dec 2019.

Vancouver:

Tan R. Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Cincinnati; 2013. [cited 2019 Dec 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378194694.

Council of Science Editors:

Tan R. Tracking of Ground Mobile Targets by Quadrotor Unmanned Aerial Vehicles. [Masters Thesis]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378194694


University of Central Florida

10. Allen, Randal. Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation.

Degree: 2009, University of Central Florida

 In this paper, an innovative cooperative navigation method is proposed for multiple Unmanned Air Vehicles (UAVs) based on online target position measurements. These noisy position… (more)

Subjects/Keywords: H-infinity; Kalman; filtering; estimation; Velocity Pursuit; Augmented Proportional Navigation; guidance; Engineering; Mechanical Engineering

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APA (6th Edition):

Allen, R. (2009). Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation. (Doctoral Dissertation). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/3933

Chicago Manual of Style (16th Edition):

Allen, Randal. “Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation.” 2009. Doctoral Dissertation, University of Central Florida. Accessed December 08, 2019. https://stars.library.ucf.edu/etd/3933.

MLA Handbook (7th Edition):

Allen, Randal. “Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation.” 2009. Web. 08 Dec 2019.

Vancouver:

Allen R. Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation. [Internet] [Doctoral dissertation]. University of Central Florida; 2009. [cited 2019 Dec 08]. Available from: https://stars.library.ucf.edu/etd/3933.

Council of Science Editors:

Allen R. Robust Estimation And Adaptive Guidance For Multiple Uavs' Cooperation. [Doctoral Dissertation]. University of Central Florida; 2009. Available from: https://stars.library.ucf.edu/etd/3933


Brigham Young University

11. Holt, Ryan S. Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems.

Degree: MS, 2007, Brigham Young University

 The ability to gather and process information regarding the condition of forest fires is essential to cost-effective, safe, and efficient fire fighting. Advances in sensory… (more)

Subjects/Keywords: augmented proportional navigation guidance; autonomous vehicle; BYU; cooperative control; coordination variables; distributed control; flight tests; forest fire monitoring; hardware results; inverse problems; perimeter surveillance; perimeter tracking; proportional navigation; road following; suitability; UAS; vision-based flight; visual servoing; Electrical and Computer Engineering

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APA (6th Edition):

Holt, R. S. (2007). Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1930&context=etd

Chicago Manual of Style (16th Edition):

Holt, Ryan S. “Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems.” 2007. Masters Thesis, Brigham Young University. Accessed December 08, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1930&context=etd.

MLA Handbook (7th Edition):

Holt, Ryan S. “Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems.” 2007. Web. 08 Dec 2019.

Vancouver:

Holt RS. Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems. [Internet] [Masters thesis]. Brigham Young University; 2007. [cited 2019 Dec 08]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1930&context=etd.

Council of Science Editors:

Holt RS. Three Enabling Technologies for Vision-Based, Forest-Fire Perimeter Surveillance Using Multiple Unmanned Aerial Systems. [Masters Thesis]. Brigham Young University; 2007. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1930&context=etd

12. [No author]. Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle.

Degree: 2015, Baylor University

 Industrial robotics, military, surveying, and delivery applications have laid a foundation for research into full autonomy of machines, including Unmanned Aerial Vehicles (UAV). This thesis… (more)

Subjects/Keywords: Potential fields. Proportional navigation. Guidance. Control. Unmanned aerial vehicle. Quad rotor. UAV. Path planning. Autonomous. Autonomy. Velocity control.

…28 Table 3.2 Added Notation for Proportional Navigation… …Potential Fields-Proportional Navigation Guidance Law develops an algorithm 5 for making… …literature review and discussion is in the introduction to Potential Fields-Proportional Navigation… …Control Block Diagram 23 CHAPTER THREE Potential Fields-Proportional Navigation Guidance Law… …we too will couple the potential field method with another method, proportional navigation… 

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APA (6th Edition):

author], [. (2015). Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9555

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):

author], [No. “Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle. ” 2015. Thesis, Baylor University. Accessed December 08, 2019. http://hdl.handle.net/2104/9555.

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

MLA Handbook (7th Edition):

author], [No. “Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle. ” 2015. Web. 08 Dec 2019.

Vancouver:

author] [. Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle. [Internet] [Thesis]. Baylor University; 2015. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2104/9555.

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

Council of Science Editors:

author] [. Integration of potential field theory and proportional navigation theory to autonomously guide an unmanned aerial vehicle. [Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9555

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

13. Robinson, Loren. General Vector Explicit - Impact Time and Angle Control Guidance.

Degree: 2015, University of Central Florida

 This thesis proposes and evaluates a new cooperative guidance law called General Vector Explicit - Impact Time and Angle Control Guidance (GENEX-ITACG). The motivation for… (more)

Subjects/Keywords: Guidance law; linear optimal control; guidance; navigation; control; missile guidance; trajectory shaping guidance law; proportional navigation; explicit guidance; linear quadratic regulator; optimal control; missile; Electrical and Computer Engineering; Electrical and Electronics; Engineering; Dissertations, Academic  – Engineering and Computer Science; Engineering and Computer Science  – Dissertations, Academic

…2.1 Geometries of Three Different Forms of Proportional Navigation . . . . . . . 13 2.2… …first guidance law presented is the well proven proportional navigation (Pro-Nav)… …common forms presented are true proportional navigation (TPN) and pure proportional… …proportional navigation (APN) is presented. APN directly accounts for target maneuvering in… …the commanded acceleration for the missile depends on which form of proportional navigation… 

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APA (6th Edition):

Robinson, L. (2015). General Vector Explicit - Impact Time and Angle Control Guidance. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/1246

Chicago Manual of Style (16th Edition):

Robinson, Loren. “General Vector Explicit - Impact Time and Angle Control Guidance.” 2015. Masters Thesis, University of Central Florida. Accessed December 08, 2019. https://stars.library.ucf.edu/etd/1246.

MLA Handbook (7th Edition):

Robinson, Loren. “General Vector Explicit - Impact Time and Angle Control Guidance.” 2015. Web. 08 Dec 2019.

Vancouver:

Robinson L. General Vector Explicit - Impact Time and Angle Control Guidance. [Internet] [Masters thesis]. University of Central Florida; 2015. [cited 2019 Dec 08]. Available from: https://stars.library.ucf.edu/etd/1246.

Council of Science Editors:

Robinson L. General Vector Explicit - Impact Time and Angle Control Guidance. [Masters Thesis]. University of Central Florida; 2015. Available from: https://stars.library.ucf.edu/etd/1246


Luleå University of Technology

14. Martinez, Lisandro. Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4.

Degree: 2009, Luleå University of Technology

Detailed analyses of galactic cosmic rays (GCR), solar proton events (SPE), and solar fluence effects have been conducted using SPENVIS and CREME96 data files… (more)

Subjects/Keywords: Technology; Space Science; technology; radiation; space radiation; space; physics; cancer; GEANT4; GRAS; ICRU sphere; AG: Antigravity; ALARA: As Low As Reasonably Achievable; ASTAR: stopping power and range tables for helium ions; BERT: Bertini Cascade Model; BNTR: Bimodal Nuclear Thermal Rocket; CERN: European Organization for Nuclear Research; CHIPS: Chiral Invariant Phase Space; CPU: Central Processing Unit; CREME96: Cosmic Ray Effects on Micro Electronics; DOSTEL: DOSimetry TELescopes; ESA: European Space Agency; GCR: Galactic Cosmic Rays; GDML: Geometry Description Markup Language; GEANT4: toolkit for the simulation of the passage of; particles through matter; GNC: Guidance Navigation and Control; GRAS: Geant4 Radiation Analysis for Space; HEP: High Energy Parameterized; ICRU: International Commission on Radiation Units and; Measurements; IMF: Interplanetary Magnetic Field; IMLEO: Initial Mass in Low Earth Orbit; INFI: Instituto Natzionale di Fisica Nuclear); ISP: Specific Impulse; ISS: International Space Station; JPL: Jet Propulsion Laboratory; LEO: Low Earth Orbit; LEP: Low Energy Parameterized; MPD: Magneto Plasma Dynamics; MULASSIS: MUlti‐:LAyered Shielding Simulation Software; NASA: National Aeronautics and Space Administration; NCRP: National Council of Radiation Protection; NEP: Nuclear Electric Propulsion; NERVA: Nuclear Engine Rocket Vehicle Application; NIST: National Institute of Standards and Technology; NTR: Nuclear Thermal Rocket; PSTAR: stopping power and range tables for protons; QGS: Quark Gluon String; S/C: Spacecraft; SPE: Solar Proton Events; SEP: Solar Electric Propulsion; SPENVIS: Space Environment Information System; TEPC: Tissue Equivalent Proportional Counter; TMI: Trans Mars Insertion; TPS: Thermal Protection System; Teknik

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

APA (6th Edition):

Martinez, L. (2009). Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-48735

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):

Martinez, Lisandro. “Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4.” 2009. Thesis, Luleå University of Technology. Accessed December 08, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-48735.

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

MLA Handbook (7th Edition):

Martinez, Lisandro. “Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4.” 2009. Web. 08 Dec 2019.

Vancouver:

Martinez L. Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4. [Internet] [Thesis]. Luleå University of Technology; 2009. [cited 2019 Dec 08]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-48735.

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

Council of Science Editors:

Martinez L. Space radiation analysis : radiation effects and particle interaction outside Earth Magnetosphere using GRAS and GEANT4. [Thesis]. Luleå University of Technology; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-48735

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

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