Integrated Guidance and Control of Homing Missiles Against Ground Fixed Targets

Abstract This paper presents a scheme of integrated guidance and autopilot design for homing missiles against ground fixed targets. An integrated guidance and control model in the pitch plane is formulated and further changed into a normal form by nonlinear coordinate transformation. By adopting the sliding mode control approach, an adaptive nonlinear control law of the system is designed so that the missile can hit the target accurately with a desired impact attitude angle. The stability analysis of the closed-loop system is also conducted. The numerical simulation has confirmed the usefulness of the proposed design scheme.

[1]  C. Tournes,et al.  INTEGRATED TERMINAL GUIDANCE AND AUTOMATIC PILOT USING SUBSPACE-STABILIZATION , 2001 .

[2]  Zhang Tian-qiao.  Passive Homing Missile's Variable Structure Proportional Navigation with Terminal Angular Constraint , 2001 .

[3]  Zha Xu.  An Integrated Approach to Guidance and Control for Aircraft Applying to Attack the Ground Fixed Targets , 2005 .

[4]  Sreenatha G. Anavatti,et al.  Observer-based adaptive guidance law considering target uncertainties and control loop dynamics , 2006, IEEE Transactions on Control Systems Technology.

[5]  Ming Xin,et al.  Integrated Guidance and Control of Missiles with Θ-D Method , 2004 .

[6]  I. A. Shkolnikov,et al.  Integrated guidance-control system of a homing interceptor - Sliding mode approach , 2001 .

[7]  Moshe Idan,et al.  Integrated sliding mode autopilot-guidance for dual-control missiles , 2005 .

[8]  Neil F. Palumbo,et al.  Integrated missile guidance and control: a state dependent Riccati differential equation approach , 1999, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328).

[9]  Nathan D. Richards,et al.  Adaptive, Integrated Guidance and Control for Missile Interceptors , 2004 .

[10]  Henrik Schiøler,et al.  Proceedings of the 2006 IEEE International Conference on Control Applications , 2006 .

[11]  Moshe Idan,et al.  Sliding-Mode Control for Integrated Missile Autopilot Guidance , 2004 .

[12]  Ernest J. Ohlmeyer,et al.  Nonlinear integrated guidance-control laws for homing missiles , 2001 .

[13]  Dongkyoung Chwa,et al.  Adaptive nonlinear guidance law considering control loop dynamics , 2003 .