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.