PCE-Based Robust Trajectory Optimization of Launch Vehicles via Adaptive Sample and Truncation-Reference-Cited by-同舟云学术

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PCE-Based Robust Trajectory Optimization of Launch Vehicles via Adaptive Sample and Truncation

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Zhengxiang¹^ORCID,Chao Tao²^ORCID,Wang Songyan³,Yang Ming⁴

Affiliation:

1. Ph.D. Candidate, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China. ORCID: .

2. Associate Professor, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China (corresponding author). ORCID: .

3. Associate Professor, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China.

4. Professor, School of Astronautics, Harbin Institute of Technology, Harbin 150001, 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.1943-5525.0001459

Reference37 articles.

1. Bataleblu A. A. and J. Roshanian. 2015. “Robust trajectory optimization of space launch vehicle using computational intelligence.” In Proc. IEEE Congress on Evolutionary Computation 3418–3425. New York: IEEE. https://doi.org/10.1109/CEC.2015.7257318.

2. Violation Learning Differential Evolution-Based hp-Adaptive Pseudospectral Method for Trajectory Optimization of Space Maneuver Vehicle

3. Solving Trajectory Optimization Problems in the Presence of Probabilistic Constraints

4. Real-Time Reentry Trajectory Planning of Hypersonic Vehicles: A Two-Step Strategy Incorporating Fuzzy Multiobjective Transcription and Deep Neural Network

5. Eldred M. C. Webster and P. Constantine. 2008. “Evaluation of non-intrusive approaches for Wiener-Askey generalized polynomial chaos.” In Proc. 10th AIAA Non-Deterministic Approaches Conf. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1892.

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1. Three-Dimensional Ascent Guidance Method for Two-Stage Solid Rocket Launch Vehicles under Multiple Constraints and Uncertainties;Journal of Aerospace Engineering;2024-01

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