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Sensitivity Methods Applied to Orbital Pursuit Evasion

Published:2015-06 Issue:6 Volume:38 Page:1118-1126
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Hafer William T.¹,Reed Helen L.²,Turner James D.²,Pham Khanh³

Affiliation:

1. Department of Aerospace Engineering, Lockheed Martin Space Systems Company, Littleton, Colorado 80210

2. Department of Aerospace Engineering, Texas A&M University, College Station, Texas 77840

3. Space Vehicles Directorate, U.S. Air Force Research Laboratory, Kirtland Air Force Base, New Mexico 87117

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000832

Reference12 articles.

1. Numerical Solution of the Three-Dimensional Orbital Pursuit-Evasion Game

2. Numerical Continuation Methods

3. A closed-form solution for the barrier in pursuit-evasion problems between two low thrust orbital spacecraft and its application

4. Near-Optimal Feedback Strategies Synthesized Using a Spatial Statistical Approach

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3. Impulsive thrust strategy for orbital pursuit-evasion games based on impulse-like constraint;Chinese Journal of Aeronautics;2024-08

4. Spacecraft Anti-reconnaissance Game based on Particle Swarm Optimization Algorithm;Advances in Astronautics Science and Technology;2024-07-11

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