The wing on the NASA F-111 transonic aircraft technology (TACT) airplane was modified to provide flexible leading and trailing edge flaps; this modified wing is known as the mission adaptive wing (MAW). A dual digital primary fly-by-wire flight control system was developed with analog backup reversion for redundancy. This report discusses the functions, design, and redundancy management of the flight control system for these flaps.
AFTI/F-111 MAW flight control system and redundancy management description
1987-02-01
Report
No indication
English
AFTI/F-16 digital flight control system experience
NTRS | 1984
|AFTI/F-111 performance flight test summary
Tema Archive | 1987
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