The invention discloses a unified design method for a suboptimal controller of an aircraft
system under multiple constraints, and the method comprises the steps: carrying out the modeling of an aircraft
system and various constraint conditions in a control process; secondly, converting the aircraft
system model into a form of an
affine nonlinear system, and representing various constraints as state inequality constraints, input amplitude inequality constraints or input time
delay constraints; then, respectively converting the state inequality constraint and the input amplitude inequality constraint into state equality constraints; meanwhile, a system containing input time
delay is converted into a system without input time
delay; then, establishing an unconstrained
augmentation system comprising a no-input time-delay system and state equality constraints; and finally, designing a sub-optimal controller based on
reinforcement learning for the unconstrained
augmentation system by adopting an execution-evaluation network framework. By means of the multi-
constraint control method, various constraints can be processed at the same time, and the multi-
constraint control method is high in universality and can be used for diversified actual application scenes.