Research Article
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⋅m2] | 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] | |
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