Optimal Guidance Solution for Impact Angle Control Based on Linearization about Collision Triangle-Reference-Cited by-同舟云学术

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Optimal Guidance Solution for Impact Angle Control Based on Linearization about Collision Triangle

Published:2011-01 Issue:1 Volume:44 Page:3909-3914
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

White Brian,Cho Hangju,Ryoo Chang-Kyung,Tsourdos Antonios

Publisher

Elsevier BV

Subject

General Medicine

Reference6 articles.

1. Closed-form optimal guidance law for missiles of time-varying velocity;Cho;Journal of Guidance, Control, and Dynamics,1996

2. Generalized vector explicit guidance;Ohlmeyer;Journal of Guidance, Control, and Dynamics,2006

3. Time-to-go weighted optimal guidance with impact angle constraints;Ryoo;IEEE Transactions on Control Systems Technology,2006

4. Time-to-go estimation using guidance command history. to appear in Proceedings of the 18th IFAC World Congress 2011;Shin,2011

5. Direct intercept guidance using differential geometry concepts;White;IEEE Transactions on Aerospace and Electronic Systems,2007

Cited by 2 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. Sliding mode control based impact angle constrained guidance with predefined convergence time;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-10-01

2. Finite-time Convergent Impact Angle Constrained Sliding Mode Guidance;IFAC-PapersOnLine;2020

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