A General Adaptive Control Structure with a Missile Application
Abstract
A general adaptive control structure is described which includes, as a special case, conventional model reference adaptive controllers. The relationships between controller parameter errors and measured signal errors are described in a form suitable for application of many parameter estimation techniques. A simplified missile pitch-axis example is given to illustrate the application of the general structure. Keywords: Adaptive control; Robust control.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1988
- Accession Number
- ADA206760
Entities
People
- Gunter Stein
- James S. Krause
Organizations
- Honeywell International, Inc.