The invention provides an
autonomous control method for fixed-point landing of an unpowered return high-speed aircraft. An attitude angle controller, a sinking rate controller, a speed controller and a transverse lateral controller are included. The attitude angle controller comprises a
pitch angle control loop, a
yaw angle control loop and a roll angle control loop; the
pitch angle loop generates a
pitch angle rate instruction Qc and outputs the
pitch angle rate instruction Qc to the
pitch angle rate loop; the
pitch angle rate loop generates an
elevator command
delta e so as to control the pitch angle of the aircraft; the
yaw angle loop is multiplied by a
gain coefficient # imgabs0 # after passing through a high-pass filter, and then a
rudder instruction
delta r is generated; the roll angle loop generates a roll angle rate instruction Pc and outputs the roll angle rate instruction Pc to the roll angle rate loop; the roll angle rate loop generates an
aileron command
delta a to control the roll angle of the aircraft; the sinking rate controller comprises a height control loop and a sinking
rate control loop; the height control loop generates a sinking rate instruction # imgabs1 # and outputs the sinking rate instruction # imgabs1 # to the sinking
rate control loop; the
subsidence rate control loop generates a pitch angle instruction theta c so as to control the
subsidence rate; a speed control loop of the speed controller outputs a speed
brake instruction # imgabs2 # so as to control the speed; the transverse lateral controller outputs a roll angle command gamma c to correct heading and offset range.