This paper addresses the design and pilot evaluation of the Core Automatic Flight Control System (AFCS) for the Reconnaissance/Attack Helicopter (RAH-66) Comanche. During the period from November 1991 through February 1992, the RAH-66 Comanche control laws were evaluated through a structured pilot acceptance test using a motion base simulator. Design requirements, descriptions of the control law design, and handling qualities data collected from ADS-33 maneuvers are presented.
Design and pilot evaluation of the RAH-66 Comanche Core AFCS
01.07.1993
Aufsatz (Konferenz)
Keine Angabe
Englisch
RAH-66 COMANCHE CORE AFCS CONTROL LAW DEVELOPMENT: DEMVAL TO EMD
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