Flight Control Law Using Composite Nonlinear Feedback Technique for a Mars Airplane-Reference-Cited by-同舟云学术

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Flight Control Law Using Composite Nonlinear Feedback Technique for a Mars Airplane

Published:2016-09 Issue:9 Volume:39 Page:2199-2204
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Liu Yanbin¹,Peng Kemao²,Lu Yuping¹,Chen Ben M.³

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

2. National University of Singapore, Singapore 117508, Republic of Singapore

3. National University of Singapore, Singapore 117576, Republic of Singapore

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G001029

Reference20 articles.

1. Design of the ARES Mars Airplane and Mission Architecture

2. Review and prospect of guidance and control for Mars atmospheric entry

3. Mars Airplane Airfoil Design with Application to ARES

4. Modeling and Control Design for the ARES Aircraft, Model-based Aerospace Challenge #1

5. On Modeling and Robust Control of ARES

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