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
01.01.2000
368903 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Robust Guidance Law for Space Interception
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