Iterative model and trajectory refinement for orbital trajectory optimization
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering; Western Michigan University; Kalamazoo, MI 49008-5343 USA
2. Department of Aerospace Engineering; University of Michigan; Ann Arbor, MI 48109-2140 USA
Funder
National Science Foundation Award
Publisher
Wiley
Subject
Applied Mathematics,Control and Optimization,Software,Control and Systems Engineering
Reference21 articles.
1. Hudson J Kolmanovsky IV Hong J et al. Iterative model and trajectory refinement for launch optimization of automotive powertrains Proceedings of 15th IFAC Workshop on Control Applications of Optimization Rimini, Italy 2012 147 151
2. Gupta R Hudson J Bloch AM Kolmanovsky IV Optimal control of manifold filling during VDE mode transitions Proceedings of the 52nd IEEE Conference on Decision and Control Florence, Italy 2013 2227 2232
3. Terminal guidance system for satellite rendezvous;Clohessy;J Aerosp Sci,1960
4. Hudson J Kolmanovsky I Iterative model refinement for orbital trajectory optimization Proceedings of 2012 AAS/AIAA Space Flight Mechanics Meeting Charleston, SC 2012 1933 1950
5. Hudson J Kolmanovsky IV Iterative model and trajectory refinement for attitude and shape control of a dumbbell spacecraft Proceedings of 2013 AAS/AIAA Astrodynamics Specialist Conference Hilton Head, South Carolina 2013 2787 2796
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