Optimal Guidance With an in Route Look-Angle Constraint
Author:
Affiliation:
1. Technology University of Vienna
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1507
Reference23 articles.
1. Stochastic Cooperative Interception Using Information Sharing Based on Engagement Staggering
2. Zarchan, P., Tactical and Strategic Missile Guidance, Vol.157, Progress in Astronautics and Aeronautics, AIAA,Washington D.C., 1994, pp.161-180.
3. Optimum intercept laws for accelerating targets.
4. Optimal intercept guidance for short-range tactical missiles
5. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories
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