Results of efforts to develop automatic control design procedures for restructurable aircraft control systems is presented. The restructurable aircraft control problem involves designing a fault tolerance control system which can accomodate a wide variety of unanticipated aircraft failure. Under NASA sponsorship, many of the technologies which make such a system possible were developed and tested. Future work will focus on developing a methodology for integrating these technologies and demonstration of a complete system.
Initial Design and Evaluation of Automatic Restructurable Flight Control System Concepts
1986
163 pages
Report
No indication
English
Active Control Technology and Restructurable Flight Controller Design
British Library Conference Proceedings | 1999
|On-line parameter estimation for restructurable flight control systems
Online Contents | 2001
|