Control design of spinning rockets based on co-evolutionary optimization
Authors:
- Ho-Il LeeHLHo-Il Lee
- Byung-Chan SunBSByung-Chan Sun
- 1 February 2001
- journal article
- research article
- Published by Elsevier in Control Engineering Practice
- Vol. 9 (2) , 149-157
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Coevolutionary augmented Lagrangian methods for constrained optimizationIEEE Transactions on Evolutionary Computation, 2000
- Coevolutionary Approaches to Structural OptimizationAIAA Journal, 1999
- A coevolutionary minimax solver and its application to autopilot design1998
- Evolutionary computation: comments on the history and current stateIEEE Transactions on Evolutionary Computation, 1997
- Aircraft controller synthesis by solving a nonconvex optimization problemJournal of Guidance, Control, and Dynamics, 1995
- Control decoupling analysis for gyroscopic effects in rolling missilesJournal of Guidance, Control, and Dynamics, 1989
- A method for computing the interval of delay values for which a differential-delay system is stableIEEE Transactions on Automatic Control, 1988
- The Generalized Root Locus (G.R.L.) method (for similar systems with antisymmetric coupling)International Journal of Control, 1976
- Dynamics of a Spinning Rocket with Varying Inertia and Applied MomentJournal of Applied Physics, 1957