Affiliation:
1. Aerospace Engineering Department, Indian Institute of Science, Bangalore, India
Abstract
This paper presents an approach to compute the optimal time-to-go and final velocity magnitude in the Generalized Explicit (GENEX) guidance. Time-to-go and final velocity magnitude are two critical input parameters in GENEX guidance implementation. Optimal time-to-go selects that optimal solution which yields less cost compared to the costs yielded by other optimal solutions. In addition to it, the input of realistic final velocity lowers the cost further. These developments relax the existing limitations of GENEX, thereby making this optimal guidance law more optimal, effective and generic.
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
3 articles.
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