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Based on nonlinear geometric theory, in this paper we propose an adaptive robust autopilot design to achieve the satisfactory tracking performance. The non-minimum phase phenomenon is a typical difficulty encountered in handing the aircraft dynamics. To cope with or relieve this undesirable intrinsic property, the output redefinition method is adopted. Here, we do not ask the underlying system to...
Based on nonlinear geometric theory, in this paper we propose an adaptive robust autopilot design to achieve the satisfactory tracking performance. The non-minimum phase phenomenon is a typical difficulty encountered in handing the aircraft dynamics. To cope with or relieve this undesirable intrinsic property, the output redefinition method is adopted. Here, we do not ask the underlying system to...
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