Time-to-go Polynomial Guidance Laws with Terminal Impact Angle/Acceleration Constraints-Reference-Cited by-同舟云学术

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Time-to-go Polynomial Guidance Laws with Terminal Impact Angle/Acceleration Constraints

Published:2011-01 Issue:1 Volume:44 Page:3915-3919
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Kim Tae-Hun,Lee Chang-Hun,Tahk Min-Jea

Publisher

Elsevier BV

Subject

General Medicine

Reference10 articles.

1. Tactical and Strategic Missile Guidance;Zarchan,1994

2. Terminal guidance for impact attitude angle constrained flight trajectories;Kim,1973

3. Apllied Optimal Control;Bryson,1975

4. Impact Angle Control for Planar Engagements;Song;IEEE Trans. on AES,1999

5. Optimal Guidance Laws with Terminal Impact Angle Constraint;Ryoo;Journal of Guidance, Control, and Dynamics,2005

Cited by 10 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. Impact-Angle-Control Guidance Law with Terminal Constraints on Curvature of Trajectory;Mathematics;2023-02-14

2. Three-stage Trajectory Planning and Control of Miniature Munition;2022 41st Chinese Control Conference (CCC);2022-07-25

3. Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed;International Journal of Aeronautical and Space Sciences;2021-04-09

4. Optimal Threshold of Intermittent Maneuver for Target Observability Improvement;International Journal of Aeronautical and Space Sciences;2020-07-07

5. Intercept Point Prediction of Ballistic Missile Defense Using Neural Network Learning;International Journal of Aeronautical and Space Sciences;2020-06-08

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