In this paper we develop an optimal mid-course strategy for guiding an interceptor. We assume that the target is outside of the sensible atmosphere and is not maneuvering throughout the engagement, and the thrust vector controlled interceptor has a fixed maneuvering time which ends well before the actual intercept. We will later extend the optimal solution to a family of guidance laws that guarantee perfect intercept for the fixed-interval maneuvering problems.
An Optimal Mid-Course Guidance Law For Fixed-Interval Propulsive Maneuvers
1993 American Control Conference ; 43-45
1993-06-01
293991 byte
Conference paper
Electronic Resource
English
Optimal Midcourse Guidance Law for Fixed-Interval Propulsive Maneuvers
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