Application of Partial Passivity-Based Control on the Guidance Problem
[1]
M. H. Shafiei, Department of Electrical and Electronic Engineering, Shiraz University of Technology, Shiraz, Iran.
In this paper, the problem of guidance law design is considered and a new guidance law is designed based on the partial passivity- based control method. The approach is based on the classification of the state variables with respect to their required stabilization properties. The resulting guidance law enables the missile to intercept highly maneuvering targets with zero miss distance within a finite interception time. Effectiveness of the proposed guidance law is demonstrated through both analysis and computer simulations.
Partial Stability, Partial Passivity-Based Control, Missile Guidance
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