Mars Entry Tracking Guidance via Quadratically Constrained Quadratic Programming and Pseudospectral Method
Author:
Affiliation:
1. Nanchang University, 330031 Nanchang, People’s Republic of China
2. Nanjing University of Aeronautics and Astronautics, 211106 Nanjing, People’s Republic of China
3. University of Tennessee, Knoxville, Tennessee 37996
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35733
Reference29 articles.
1. Apollo-derived Mars precision lander guidance
2. Entry Guidance for the 2011 Mars Science Laboratory Mission
3. Comparison of the Effects of Velocity and Range Triggers on Trajectory Dispersions for the Mars 2020 Mission
4. Adaptive entry guidance for the Tianwen-1 mission
5. Design and Evaluation of an Acceleration Guidance Algorithm for Entry
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