An enhanced anti-disturbance guidance scheme for powered descent phase of Mars landing under actuator fault
Author:
Affiliation:
1. School of Automation Science and Electrical Engineering, Beihang University, Beijing, China
2. Beijing Advanced Innovation Center for Big Data-based Precision Medicine, Beihang University, Beijing, China
Abstract
Funder
Program for Changjiang Scholars and Innovative Research Team
Publisher
SAGE Publications
Subject
Artificial Intelligence,Computer Science Applications,Software
Link
http://journals.sagepub.com/doi/pdf/10.1177/1729881418759889
Reference35 articles.
1. Mars Science Laboratory Simulations for Entry, Descent, and Landing
2. Assessment of Environments for Mars Science Laboratory Entry, Descent, and Surface Operations
3. Validation of Mars Global Reference Atmospheric Model (Mars-GRAM 2001) and planned new features
4. Mars Science Laboratory Entry, Descent, and Landing System Development Challenges
5. Reconstruction of Atmospheric Properties from Mars Science Laboratory Entry, Descent, and Landing
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1. A Novel Multiplicative Fault Observer for actuators of Satellite Attitude Control System;2022 5th International Symposium on Autonomous Systems (ISAS);2022-04-08
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