The invention provides an
airplane Herbst maneuvering control method, and the method is based on a dynamic reverse idea. A designed controller comprises an outer ring flight path controller and an inner ring posture controller. The outer ring flight path controller calculates an
attack angle instruction, a sideslip angle instruction, an instruction of a roll angle about the
velocity vector and an engine thrust instruction for controlling the velocity of an
airplane for achieving the set maneuvering light path. The inner ring posture controller controls the
attack angle, the sideslip angle and the roll angle about the
velocity vector through operating a pneumatic control plane of the
airplane and a thrust vector. The method obtains an analytical expression of the outer ring flight path controller, wherein an
attack angle instruction controller has an I controller form in a
PID controller, and avoids the complex numerical calculation. Meanwhile, the method can adjust the solving precision of the control instruction, and is more suitable for the design of an airplane Herbst maneuvering controller in the
engineering field.