Research on Aircraft Cooperative Formation Control Based on Neural Network
Aiming at the guidance and control problem of aircraft cooperative formation based on Leader-Follower structure, the guidance loop and control loop of the side-slip turning aircraft were analyzed and designed. Firstly, relative motion coordinate system is defined in inertial space, and relative moti...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Control and Information Technology
2019-01-01
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| Series: | Kongzhi Yu Xinxi Jishu |
| Subjects: | |
| Online Access: | http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.006 |
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| Summary: | Aiming at the guidance and control problem of aircraft cooperative formation based on Leader-Follower structure, the guidance loop and control loop of the side-slip turning aircraft were analyzed and designed. Firstly, relative motion coordinate system is defined in inertial space, and relative motion model is established. Secondly, the acceleration information of a Leader is taken as disturbance, and the formation guidance law is designed based on sliding mode variable structure and neural network theory. Considering the problem of overload saturation, the rules for determining guidance parameters are given. Finally, the control system is designed and the stability of the guidance and control system is proved. The simulation results show that the designed guidance and control system can construct and maintain the desired formation quickly and accurately. |
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| ISSN: | 2096-5427 |