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International Conference on Advanced Computer Theory and Engineering (ICACTE 2009)

Xie Yi
Xie Yi
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ASME Press
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The challenge and control problem of static unstable missiles were presented. The steady-state benefits of static instability were illustrated, while the corresponding control challenge was described by the characteristic lag of airframe and the increment of necessary control usage. Control limitation led by unstable zero-pole pair was analyzed for preliminary design and evaluation. Linear control strategy was examined wherein the three loop acceleration autopilots was developed using an optimal control approach combined with frequency domain constraint. The weights selection and relation with system performance were detailed. Then the nonlinear backstepping recursive method was detailed. The results show that the actuator...

Key Words
1 Introduction
2. Missile Longitudinal Dynamics
3 Acceleration Autopilot Design
4. Conclusion
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