Gaussian Distribution–Based Control Vector Parameterization Method for Constrained Hypersonic Vehicle Reentry Trajectory Optimization-Reference-Cited by-同舟云学术

Gaussian Distribution–Based Control Vector Parameterization Method for Constrained Hypersonic Vehicle Reentry Trajectory Optimization

Published:2023-11 Issue:6 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Ping¹^ORCID,Liu Hang²,Chen Tianyi²,Liu Xinggao³

Affiliation:

1. Associate Professor, College of Automation, Chongqing Univ. of Posts and Telecommunications, Chongqing 400065, China (corresponding author). ORCID: .

2. Graduate Student, College of Automation, Chongqing Univ. of Posts and Telecommunications, Chongqing 400065, China.

3. Professor, College of Control Science and Engineering, Zhejiang Univ., Hangzhou 310027, 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/JAEEEZ.ASENG-4711

Reference27 articles.

1. Practical Methods for Optimal Control and Estimation Using Nonlinear Programming

2. Dynamic optimization using a wavelet based adaptive control vector parameterization strategy

3. A review of optimization techniques in spacecraft flight trajectory design

4. Review of control and guidance technology on hypersonic vehicle

5. Introduction to Computational Intelligence

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