The functional mockup test of the flight control system of ASKA with the stability and control augmentation systems is described. The tests made included software verification, simulated failure effects testing, closed loop test, and piloted simulation test. The results show that the functions and performance of the control system are satisfactory for flight safety of ASKA.
Functional Mock-Up Test of the Flight Control System of the NAL (National Aerospace Laboratory) QSTOL Research Aircraft ASKA
1988
64 pages
Report
No indication
English
Functional Mock-Up Tests for Flight Control System of the NAL QSTOL Research Aircraft ‘ASKA’
SAE Technical Papers | 1991
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