Optimal and Constrained-Optimal Control of a Flexible Launch Vehicle
Authors:
- 1 June 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (6) , 796-799
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- On the determination of the optimal constant output feedback gains for linear multivariable systemsIEEE Transactions on Automatic Control, 1970
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- On an iterative technique for Riccati equation computationsIEEE Transactions on Automatic Control, 1968
- Sub-optimal Time-variable Feedback Control of Linear Dynamic Systems with Random Inputs†International Journal of Control, 1966
- An application of the quadratic penalty function criterion to the determination of a linear control for a flexible vehicleAIAA Journal, 1965
- An Automatic Method for Finding the Greatest or Least Value of a FunctionThe Computer Journal, 1960