Mars entry guidance for mid-lift-to-drag ratio vehicle with control constraints-Reference-Cited by-同舟云学术

Mars entry guidance for mid-lift-to-drag ratio vehicle with control constraints

Published:2020-12 Issue: Volume:107 Page:106361
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Gong Youmin^ORCID,Guo Yanning^ORCID,Ma Guangfu,Guo Minwen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. Mid-lift-to-drag ratio rigid vehicle control system design and simulation for human Mars entry;Johnson,2018

2. A rigid mid lift-to-drag ratio approach to human Mars entry, descent, and landing;Sostaric,2017

3. Mid lift-to-drag rigid vehicle 6-dof performance for human Mars entry, descent, and landing: a fractional polynomial powered descent guidance approach;Johnson,2020

4. Technology development for human exploration of Mars;Moore;Acta Astronaut.,2010

5. Automatic load relief numerical predictor-corrector guidance for low l/d vehicles return from low earth orbit;Zhang;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2015

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