Guidance algorithm for impact time, angle, and acceleration control under varying velocity condition-Reference-Cited by-同舟云学术

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Guidance algorithm for impact time, angle, and acceleration control under varying velocity condition

Published:2022-04 Issue: Volume:123 Page:107462
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Wanqing,Chen Wanchun,Li Jinglin,Yu Wenbin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. A general, explicit, optimizing guidance law for rocket-propelled spaceflight;Cherry,1964

2. Applied Optimal Control;Bryson,1969

3. Tactical and Strategic Missile Guidance;Zarchan,2012

4. Generalized vector explicit guidance;Ohlmeye;J. Guid. Control Dyn.,2006

5. Optimal terminal guidance for exoatmospheric interception;Yu;Chin. J. Aeronaut.,2016

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1. Data-Driven-Method-Based Guidance Law for Impact Time and Angle Constraints;Aerospace;2024-07-01

2. Sinusoidal Guidance;Journal of Guidance, Control, and Dynamics;2023-11-08

3. Impact time control guidance law with time-varying velocity based on deep reinforcement learning;Aerospace Science and Technology;2023-11

4. 3-D Impact Time and Angle Control Guidance Law Based on Sliding Mode without Speed Control;Journal of Circuits, Systems and Computers;2023-10-06

5. Impact angle constraint guidance law using fully-actuated system approach;Aerospace Science and Technology;2023-05

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