The invention relates to an aircraft overload
loop design method for providing damping by adopting
angular acceleration and belongs to the technical field of aircraft control. According to the method,an angular
accelerometer is adopted to measure the
yaw angular acceleration of an aircraft to provide damping for an overload outer loop, then an
accelerometer is adopted to measure the
linear acceleration of the aircraft to obtain lateral overload; the lateral overload is compared with an expected overload instruction, and therefore, an overload
error signal is obtained; integration is performedon the overload
error signal twice, so that an overload error comprehensive integration
signal can be formed, so that a conversion
static error problem between the overload instruction and an attitude instruction can be eliminated; the
nonlinear transformation signal of an aircraft attitude
angular acceleration signal, the proportional signal of a
yaw rate and the secondary
nonlinear transformation signal of an aircraft angular speed signal are introduced to form the damping signal of the overload loop, and the damping signal is output to an attitude stabilization loop, so that the
control objective of overload tracking can be realized. With the method adopted, the problems of
static error and insufficient damping of traditional
overload control can be solved.