Impact-Point-Based Guidance of a Spinning Artillery Rocket Using Canard Cyclic Control

Author:

Yang Shu1

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 7 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. The Active Disturbance Rejection Control Method for Stabilizing the Roll Channel in High-Dynamic Missiles;2023 China Automation Congress (CAC);2023-11-17

2. Guidance and Control of Spin-Stabilized Projectiles Based on Super Twisting Algorithm;Journal of Guidance, Control, and Dynamics;2023-03

3. Thrust optimization in the trajectory control strategy for ballistic rocket;MACHINE LEARNING AND INFORMATION PROCESSING: PROCEEDINGS OF ICMLIP 2023;2023

4. Guidance and Control of a Spinning 155mm Artillery Shell;2022 17th International Conference on Emerging Technologies (ICET);2022-11-29

5. Three-Dimensional Guidance Law Mimicking Realistic Ballistic Trajectories;Journal of Guidance, Control, and Dynamics;2022-09

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