This paper proposes a method of using multi-controllers to control supermaneuverable air- craft. A nonlinear dynamic-inversion controller is used for supermaneuver. A gain-scheduled con- troller is used for routine maneuver. A switch algorithm is designed to switch the controllers. The flight envelopes of the controllers are different but have a common area in which the controllers are switched from one to the other. In the common area, some special boundaries are selected to decide switch conditions.
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