26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-5.7.3

INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT

H. S. Shin, T. W. Hwang*, A. Tsourdos**, B. A. White**, M. J. Tahk
KAIST, Korea; *Agency for Defence Development, Korea; **Cranfield Univ., UK

Keywords: Integrated guidance and control, Interception, Terminal angle constraint, Lyapunov candidate function, Backstepping, Disturbance observer

This paper proposed integrated design of missile guidance and control for manoeuvring targets. To control engagement geometry, impact-angle-control guidance is analysed in two dimensional geometry. The integrated backstepping design with disturbance observer is interpreted in view of stability and robustness. The performance of the algorithm is verified via numerical simulation.

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