Control Law Design for Aircraft Autopilot Based on Particle Swarm Optimization Method-Reference-Cited by-同舟云学术

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Control Law Design for Aircraft Autopilot Based on Particle Swarm Optimization Method

Published:2023-05-19 Issue: Volume: Page:
ISSN:
Container-title:2023 2nd International Symposium on Aerospace Engineering and Systems (ISAES)
language:
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Author:

Wang Jianqi¹,Wang Dongmei²,Zhang Yunyuan³

Affiliation:

1. Guilin University of Aerospace Technology,Key Laboratory of Unmanned Aerial Vehicle Telemetry,Guilin,P. R. China

2. Guilin University of Aerospace Technology,Library Information Center,Guilin,P. R. China

3. Guilin University of Aerospace Technology,School of Electronic Information and Automation,Guilin,P. R. China

Funder

National Natural Science Foundation of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10280773/10281200/10281284.pdf?arnumber=10281284

Reference20 articles.

1. An overview on development of miniature unmanned rotorcraft systems

2. Exact convex relaxation for optimal flight of aerodynamically controlled missiles

3. Three-loop autopilot design and simulation

4. Rapid Homing Guidance Using Jerk Command and Time-Delay Estimation Method

5. Characteristics and Key Technologies of the Fifth Generation Air-to-air Missile;Huiyao;Aeronautical science and Technology [J],2011

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