The invention discloses a dynamic
attack angle amplitude limiting method for reducing
missile body overload when aerodynamic configuration changes. The method dynamically limits the amplitude the
attack angle of the
missile in order to reduce
missile body overload when aerodynamic configuration changes. The method for dynamically limiting the amplitude of the
attack angle of the missile comprises: S1, computing a maximum attack angle amplitude value of the missile in a before-separation stable process and a after-separation stable process and a maximum attack angle amplitude value of the missile when aerodynamic configuration changes, and variation ranges of the attack angle and the
flight speed of the missile; S2, determining a attack angle limiting
amplitude function varying with the
flight speed of the missile; S3, determining a function relationship between a maximum lift coefficient, attack angle limiting amplitude value, and the
flight speed; and S4, acquiring the reference area and the
mass of the missile, the flight
dynamic pressure, the flight speed, and the trajectory inclination angle of the missile at the
current time so as to determine the upper
limit value and the
lower limit value of a overload amplitude
limiter at a
current time. The method may determine an optimum attack angle limiting amplitude value according to the real-time flight state of the missile and reduce missile body overload when aerodynamic configuration changes.