Efficient Trajectory Planning for Solid Rocket-Powered Launch Vehicles based on the Newton-Kantorovich/Pseudospectral Approach-Reference-Cited by-同舟云学术

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Efficient Trajectory Planning for Solid Rocket-Powered Launch Vehicles based on the Newton-Kantorovich/Pseudospectral Approach

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
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Author:

Cheng Xiaoming X.¹,Li Huifeng¹,Zhang Ran¹,Zhang Zhenning¹

Affiliation:

1. Beihang University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2231

Reference26 articles.

1. Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization

2. Stability analysis of autonomous space systems in the presence of large disturbances: A Lyapunov-based constrained control strategy

3. Robust adaptive dynamic surface control design for a flexible air-breathing hypersonic vehicle with input constraints and uncertainty

4. Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance Algorithm

5. Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Integrated design of sun-synchronous orbit and launch vehicle trajectory for operationally responsive space;Journal of Physics: Conference Series;2023-12-01

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