In space interception, a linear time-varying model is established to describe the missile-target related line-of-sight (LOS) motion, where the guidance parameter variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results obtained demonstrate the effectiveness of the presented guidance method.
Robust guidance law for space interception
2000-01-01
368903 byte
Conference paper
Electronic Resource
English
Robust Guidance Law for Space Interception
British Library Conference Proceedings | 2000
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