Optimality of Proportional Navigation
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N.Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. Linear feedback solutions for minimum effort interception, rendezvous, and soft landing
2. Optimum intercept laws for accelerating targets.
3. Optimum rendezvous intercept, and injection.
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