关键词: 非线性解耦控制, 鲁棒控制, 机动飞行

Abstract:

The design of a maneuverable flight command tracking system using nonlinear dynamic inversion is briefly introduced at first. And then a robust controller to improve the robustness of dynamic inversion is designed using the method of μ analysis and synthesis. The detailed design process and results are presented. Simulations show that the robust dynamic inversion controller yields good results.

Key words: nonlinear control, r obust cont rol, maneuver s