Downrange Estimation Based on Powered Explicit Guidance for Pinpoint Lunar Landing-Reference-Cited by-同舟云学术

Downrange Estimation Based on Powered Explicit Guidance for Pinpoint Lunar Landing

Published:2022-03 Issue:2 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang Haofan¹^ORCID,Zhang Honghua²,Wang Zeguo³,Wang Zhiwen³

Affiliation:

1. Ph.D. Candidate, First Research Dept., Beijing Institute of Control Engineering, Beijing 100190, China (corresponding author). ORCID: .

2. Professor, Chief Engineer Office, Beijing Institute of Control Engineering, Beijing 100190, China.

3. Engineer, First Research Dept., Beijing Institute of Control Engineering, Beijing 100190, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001383

Reference37 articles.

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

3. Robust Nonlinear Optimal Solution to the Lunar Landing Guidance by Using Neighboring Optimal Control

4. Banerjee, A., and R. Padhi. 2020. “Multi-phase MPSP guidance for lunar soft landing.” Trans. Indian Natl. Acad. Eng. 5 (1): 61–74. https://doi.org/10.1007/s41403-020-00090-1.

5. Bryson, A. E. 1975. Applied optimal control: Optimization, estimation and control. Boca Raton, FL: CRC Press.

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