Abstract
This paper concerns the cross-linking between aircraft attitude control system and actuator, proposes a new method of designing aircraft attitude controller while considering the characteristics and constraints of actuator. The mathematical model of actuator is deduced and a servo controller is designed. Considering the characteristic and constraints of actuator, model of attitude control system is presented based on general dynamic analysis of aircraft. Under the multi-constraints of both dynamic quality and frequency domain margin, multi-objective evolutionary optimization (improved genetic algorithm) is implemented to adjust parameters of the proposed attitude controller.
| Original language | English |
|---|---|
| State | Published - 2018 |
| Event | CSAA/IET International Conference on Aircraft Utility Systems, AUS 2018 - Guiyang, China Duration: 19 Jun 2018 → 22 Jun 2018 |
Conference
| Conference | CSAA/IET International Conference on Aircraft Utility Systems, AUS 2018 |
|---|---|
| Country/Territory | China |
| City | Guiyang |
| Period | 19/06/18 → 22/06/18 |
Keywords
- Actuator
- Aircraft attitude control system
- Crosslinking
- Improved genetic algorithm
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