CAJ | 학술논문

飞行品质标准对耦合现象有着明确的限制和评定，为了实现飞机的解耦控制，本文基于模型跟踪技术进行了解耦控制律的设计。首先构建了非耦合的目标模型，其次利用模型跟踪对非耦合模型完满复现，实现了解耦目的，最后分析了模型反馈增益和舵回路对解耦控制律的影响并提出了解决方法。仿真结果表明：利用模型跟踪控制技术可实现飞机通道之间的解耦，且该方法简单明了，易于工程实现。
비행품질표준대우합현상유착명학적한제화평정，위료실현비궤적해우공제，본문기우모형근종기술진행료해우공제률적설계。수선구건료비우합적목표모형，기차이용모형근종대비우합모형완만복현，실현료해우목적，최후분석료모형반궤증익화타회로대해우공제률적영향병제출료해결방법。방진결과표명：이용모형근종공제기술가실현비궤통도지간적해우，차해방법간단명료，역우공정실현。
There is clear limitation and evaluation about coupling in the standard of flying qualities. The decou- pling control law is designed by using the model following technique in order to realize the decoupling control of an aircraft. First, the goal-model which is uncoupling is created. Then, the uncoupling responses are repro- duced by the model following loop and realize the decoupling control. Finally, the influence of the feedback gain and servo actuator loop is analyzed. The simulation results show that the decoupling between plane channels can be realized by using model-following control technique, and this method is easy to realize in the project.