Optimal Guidance for Quasi-planar Lunar Ascent-Reference-Cited by-同舟云学术

Optimal Guidance for Quasi-planar Lunar Ascent

Published:2011-07-01 Issue:2 Volume:151 Page:353-372
ISSN:0022-3239
Container-title:Journal of Optimization Theory and Applications
language:en
Short-container-title:J Optim Theory Appl

Author:

Hull David G.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Management Science and Operations Research,Control and Optimization

Link

http://link.springer.com/content/pdf/10.1007/s10957-011-9884-5.pdf

Reference17 articles.

1. Miele, A.: General variational theory of the flight paths of rocket-powered aircraft, missiles, and satellite carriers. Acta Astronaut. 4, 264–288 (1958)

2. Lawden, D.F.: Necessary conditions for optimal rocket trajectories. Q. J. Mech. Appl. Math. 12, 476–487 (1959)

3. Breakwell, J.V.: The optimization of trajectories. SIAM J. 7, 215–247 (1959)

4. Leitmann, G.: On a class of variational problems in rocket flight. J. Aerosp. Sci. 26, 586–591 (1959)

5. Yang, T.L.: Optimal control for a rocket in a three-dimensional central force field, Report No. TM 69-2011-2, BELLCOMM (1969)

Cited by 23 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. Abort Guidance During Lunar Powered Descent;Journal of Guidance, Control, and Dynamics;2024-01-18

2. Optimal Powered Descent Guidance Under Thrust Pointing Constraint;Journal of Guidance, Control, and Dynamics;2023-04

3. Propellant-Optimal Powered Descent Guidance Revisited;Journal of Guidance, Control, and Dynamics;2023-02

4. Propellant-Optimal Powered Descent Guidance Revisited;AIAA SCITECH 2023 Forum;2023-01-19

5. Lunar ascent control using explicit guidance and slidng mode techniques;2022 China Automation Congress (CAC);2022-11-25