Control variables for finite element solution of missile trajectory optimization
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
2. LORAL Vought Systems, Dallas, Texas 75265-5907
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.21528
Reference8 articles.
1. Weak Hamiltonian finite element method for optimal control problems
2. Finite element solution of optimal control problems with state-control inequality constraints
3. Finite element method for optimal guidance of an advanced launch vehicle
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1. Optimization in simulations of human movement planning;International Journal for Numerical Methods in Engineering;2011-02-21
2. Finite Elements in Time: A Direct Transcription Method for Optimal Control Problems;AIAA/AAS Astrodynamics Specialist Conference;2010-06-14
3. The solution of a launch vehicle trajectory problem by an adaptive finite-element method;Computer Methods in Applied Mechanics and Engineering;2001-06
4. Deferred-Correction Optimal Control with Applications to Inverse Problems in Flight Mechanics;Journal of Guidance, Control, and Dynamics;2001-01
5. Solving Optimal Control Problems Using hp-Version Finite Elements in Time;Journal of Guidance, Control, and Dynamics;2000-01
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