Throttled explicit guidance for pinpoint landing under bounded thrust acceleration-Reference-Cited by-同舟云学术

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Throttled explicit guidance for pinpoint landing under bounded thrust acceleration

Published:2020-11 Issue: Volume:176 Page:438-454
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ito T.,Sakai S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Lunar reconnaissance orbiter overview: the instrument suite and mission;Chin;Space Sci. Rev.,2007

2. An overview of the mars reconnaissance orbiter (MRO) science mission;Zurek;J. Geophys. Res.,2007

3. The kaguya mission overview;Saito;Space Sci. Rev.,2010

4. A powered descent guidance algorithm for mars pinpoint landing;Acikmese,2005

5. Performance trades for mars pinpoint landing;Wolf,2006

Cited by 5 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. Chance-Constrained Control for Safe Spacecraft Autonomy: Convex Programming Approach;2024 American Control Conference (ACC);2024-07-10

2. Hybrid Zero-Effort-Miss/Zero-Effort-Velocity Guidance for Powered Descent Phase;Journal of Guidance, Control, and Dynamics;2024-05

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

4. Multi-constrained feedback guidance for mars pinpoint soft landing using time-varying sliding mode;Advances in Space Research;2022-10

5. Throttled Explicit Guidance to Realize Pinpoint Landing Under a Bounded Thrust Magnitude;Journal of Guidance, Control, and Dynamics;2021-04

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