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21st Southern California Nonlinear Control Workshop
State Limiter for Model Following Control Systems
Ross Gadient
Advisor: Petros Ioannou
We present state-limiting augmentation applied to a baseline dynamic inversion control design. While the baseline dynamic inversion control law is designed to meet robustness and performance requirements throughout a flight envelope, the state-limiting component protects the system trajectories from leaving an allowable subset in the system state space. The proposed design is applied to the X-48B blended-wing-body (BWB) aircraft in both the longitudinal and lateral/directional axes, with simulation results included.
Advisor: Petros Ioannou
We present state-limiting augmentation applied to a baseline dynamic inversion control design. While the baseline dynamic inversion control law is designed to meet robustness and performance requirements throughout a flight envelope, the state-limiting component protects the system trajectories from leaving an allowable subset in the system state space. The proposed design is applied to the X-48B blended-wing-body (BWB) aircraft in both the longitudinal and lateral/directional axes, with simulation results included.