Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile-Reference-Cited by-同舟云学术

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Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile

Published:2020-08 Issue: Volume: Page:
ISSN:
Container-title:2020 IEEE Conference on Control Technology and Applications (CCTA)
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Author:

Thai Sovanna,Theodoulis Spilios,Roos Clement,Biannic Jean-Marc,Proff Michael

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9200884/9206152/09206311.pdf?arnumber=9206311

Cited by 6 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. Back Calculation Anti-Windup Strategy for the Pitch Control of a Launch Vehicle Autopilot;2023 Second International Conference on Trends in Electrical, Electronics, and Computer Engineering (TEECCON);2023-08-23

2. A guidance and control design with reduced information for a dual-spin stabilized projectile;Defence Technology;2023-07

3. Robust gain-scheduled autopilot design with anti-windup compensation for a guided projectile;CEAS Aeronautical Journal;2023-07

4. L1 Adaptive Augmentation of an Incremental Nonlinear Dynamic Inversion Autopilot for Dual-Spin Guided Projectiles;AIAA SCITECH 2023 Forum;2023-01-19

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

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