Predictive guidance algorithms for maximal downrange maneuvrability with application to low-lift re-entry-Reference-Cited by-同舟云学术

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Predictive guidance algorithms for maximal downrange maneuvrability with application to low-lift re-entry

Published:2009-04 Issue:7-8 Volume:64 Page:770-777
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kozynchenko Alexander I.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. Survey of atmosphere re-entry guidance and control methods;Wingrove;AIAA Journal,1963

2. Trajectory control for a low-lift re-entry vehicle;Roenneke;Journal of Guidance, Control, and Dynamics,1993

3. Atmospheric re-entry control for low lift/drag vehicles;Cavallo;Journal of Guidance, Control, and Dynamics,1996

4. Terminal guidance for an unpowered reusable launch vehicle with bank constraints;Kluever;Journal of Guidance, Control, and Dynamics,2007

5. Feasible trajectory generation for atmospheric entry guidance;Leavitt;Journal of Guidance, Control, and Dynamics,2007

Cited by 3 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. Mars atmospheric entry guidance for optimal terminal altitude;Acta Astronautica;2019-02

2. Analysis of predictive entry guidance for a Mars lander under high model uncertainties;Acta Astronautica;2011-01

3. Enhancing the manoeuvring capabilities of a lunar landing module using predictive guidance algorithms;Acta Astronautica;2010-08

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