Two-Phase Zero-Effort-Miss/Zero-Effort-Velocity Guidance for Mars Landing
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. Iowa State University, Ames, Iowa 50010-2271
Funder
National Natural Science Foundation of China
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
Reference36 articles.
1. Mars Exploration Entry, Descent, and Landing Challenges
2. Minimum-Fuel Powered Descent for Mars Pinpoint Landing
3. Entry Guidance Performance for Mars Precision Landing
4. Convex Programming Approach to Powered Descent Guidance for Mars Landing
5. Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization
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