High-Precision Adaptive Predictive Entry Guidance for Vertical Rocket Landing
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
The National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference11 articles.
1. Advancing Supersonic Retro-Propulsion Technology Readiness: Infrared Observations of the SpaceX Falcon 9 First Stage
2. Propellant-Optimal Powered Descent Guidance
3. Adaptive Powered Descent Initiation and Fuel-Optimal Guidance for Mars Applications
4. A robust predictor–corrector entry guidance
5. Entry Guidance: A Unified Method
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