Optimal Terminal Guidance with Constraints at Final Time
Author:
Affiliation:
1. Western Kentucky University, Bowling Green, Ky.
2. U.S. Army Missile Research and Development Command, Redstone Arsenal, Ala.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57212
Reference10 articles.
1. Velocity of bodies powered by rapidly discharged cold-gas thrusters
2. Velocity of bodies powered by diatomic cold-gas thrusters
3. 3Hamming, R.W.,Introduction to Applied Numerical Analysis, 1st ed.McGraw-Hill, New York, 1971, pp.184-186(Simpson's formula).
4. Missile Guidance by Three‐Dimensional Proportional Navigation
5. Fundamentals of proportional navigation
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