Autopilot Design Method for the Blended Missile Based on Model Predictive Control

Table 1

Missile’s overall parameters.

Missile’s takeoff mass [kg]	255
Missile’s full-length [m]	4.86
Missile’s diameter [m]	0.317
Distance between missile head and center of mass [m]	2.569
Moment of inertia [kg⋅m^2]	3.03, 306.3, 306.3
Lateral force provided by individual jets [N]	2200
Distance between jet ring center and center of mass [m]	1.26
Range of angle of attack [rad]
Range of pitch angular velocity [rad/s]
Range of elevator deflection [rad]