Dynamic Tube Model Predictive Control for Powered-Descent Guidance-Reference-Cited by-同舟云学术

Dynamic Tube Model Predictive Control for Powered-Descent Guidance

Published:2022-11 Issue:6 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cheng Long¹,Wen Hao²^ORCID,Kang Junjie³,Jin Dongping⁴

Affiliation:

1. Lecturer, School of Aeronautical Manufacturing Engineering, Nanchang Hangkong Univ., Nanchang 330063, PR China.

2. Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China (corresponding author). ORCID: .

3. Associate Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China.

4. Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001487

Reference39 articles.

1. Lossless convexification of a class of optimal control problems with non-convex control constraints

2. Convex Programming Approach to Powered Descent Guidance for Mars Landing

3. CasADi: a software framework for nonlinear optimization and optimal control

4. Mars exploration rovers entry, descent, and landing trajectory analysis

5. Customized Real-Time Interior-Point Methods for Onboard Powered-Descent Guidance

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