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Authors
Dwivedi, Prasiddha Nath; Bhattacharyaa, Abhijit; Padhi, Radhakant

Digital Object Identifier (DOI)
10.3182/20080706-5-KR-1001.00600

Page Numbers:
3550-3555

Index Terms
Model reference adaptive control

Abstract
For a homing interceptor, suitable initial condition must be achieved by mid course guidance scheme for its maximum effectiveness. To achieve desired end goal of any mid course guidance scheme, two point boundary value problem must be solved online with all realistic constrain. A Newly developed computationally efficient technique named as MPSP (Model Predictive Static Programming) is utilized in this paper for obtaining suboptimal solution of optimal mid course guidance. Time to go uncertainty is avoided in this formulation by making use of desired position where midcourse guidance terminate and terminal guidance takes over. A suitable approach angle towards desired point also can be specified in this guidance law formulation. This feature makes this law particularly attractive because warhead effectiveness issue can be indirectly solved in mid course phase.

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