The philosophy and techniques adopted for the flight testing of the swing-wing Tornado aircraft digitally based self-contained all-weather NAV/ATTACK avionics system are presented. The subsystems for navigation, displays, flight control, weapon aiming, computing, and data transmission are described. The development organization and development program system are described briefly. The stage 3 flight trials program is detailed.
The Philosophy Adopted for the Flight Testing of the Panavia Tornado Avionics System in Hack Aircraft
1977
17 pages
Report
No indication
English
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