NASA NTRS ยท 19780018838
On reliable control system designs
Abstract
A mathematical model for use in the design of reliable multivariable control systems is discussed with special emphasis on actuator failures and necessary actuator redundancy levels. The model consists of a linear time invariant discrete time dynamical system. Configuration changes in the system dynamics are governed by a Markov chain that includes transition probabilities from one configuration state to another. The performance index is a standard quadratic cost functional, over an infinite time interval. The actual system configuration can be deduced with a one step delay. The calculation of the optimal control law requires the solution of a set of highly coupled Riccati-like matrix difference equations. Results can be used for off-line studies relating the open loop dynamics, required performance, actuator mean time to failure, and functional or identical actuator redundancy, with and without feedback gain reconfiguration strategies.
Keep this discovery
Explore connections, maps & timelines
Birdwell, J. D.. 1978-05-01. On reliable control system designs. https://ntrs.nasa.gov/citations/19780018838
Cite the original work for its findings. Save a collection to share your selection of sources.