Development of a reconfigurable helicopter flight control system
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Development of a reconfigurable helicopter flight control system by Pavan Rajagopal

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Published by National Library of Canada in Ottawa .
Written in English


Book details:

Edition Notes

Thesis (M.A.Sc.)--University of Toronto, 1992.

SeriesCanadian theses = Thèses canadiennes
The Physical Object
FormatMicroform
Pagination4 microfiches : negative.
ID Numbers
Open LibraryOL15136844M
ISBN 100315872187
OCLC/WorldCa46536389

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Repairing Flight Control System, Propulsion-Controlled Aircraft, and Intelligent Flight Control programs as well as the F-8 FBW demonstrator that flight tested a number of technologies File Size: KB. An actuator geometry that enables reconfigurable helicopter flight control is presented, and, from this, reconfigurable flight-control methods are developed to accommodate main rotor . A neural-network-based direct adaptive control approach to the problem of reconfigurable flight control is described. The control law was first tested using a model of a tailless fighter aircraft. Enns, R., & Si, J. (). Reconfigurable helicopter flight control methods for main rotor actuator AIAA Guidance, Navigation, and Control Conference and Exhibit (AIAA Guidance, Author: Russell Enns, Jennie Si.

Flight tests of reconfigurable flight control systems were performed with an F aircraft during the Self-Reparing Flight Control System (SRFCS) programme (Corvin et al., ) and in the. The Aerial Reconfigurable Embedded System (ARES) was a concept for an unmanned VTOL flight module that can transport various payloads. The concept started as the TX (Transformer) in for a terrain-independent transportation system centered on a ground vehicle that could be configured into a VTOL air vehicle and carry four ' primary function was the same as TX, to use flight . A Unique Approach to the Development of a Light Helicopter Automatic Flight Control System The requirements and implementation of the Enstrom Cruise-A-Long flight control Author: Donald R. Korte, Robert Bakotich.   Reconfigurable Intelligent Control Architecture of a Small-Scale Unmanned Helicopter This paper deals with the design and development of a layered architectural framework that addresses the issue arising in autonomous intelligent control systems. The architecture consists of two layers. Autopilot for Reconfigurable Flight Control System.

Design of helicopter automatic flight control system [Schrage, D. P] on *FREE* shipping on qualifying offers. Design of helicopter automatic flight control systemAuthor: D. P Schrage. The FCC hosts the flight control law code. The FCC is a single-channel system. A basic set of software elements provides a standardized interface to sensor data, pilot inputs and aircraft File Size: KB. A typical FTR control system would consist of actuators, sensors, computer systems, data acquisition systems, and often mechanical, hydraulic, pneumatic, electronic devices and . Reconfigurable Intelligent Control Architecture of a Small-Scale Unmanned Helicopter This paper deals with the design and development of a layered architectural framework that .