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 accommodate 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
1986-06-01
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
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