The flight-acceptance test results obtained during the acceptance tests of the V/STOLAND (versatile simplex digital avionics system) digital avionics system on a Bell UH-1H helicopter in 1977 at Ames Research Center are presented. The system provides navigation, guidance, control, and display functions for NASA terminal area VTOL research programs and for the Army handling qualities research programs at Ames Research Center. The acceptance test verified system performance and contractual acceptability. The V/STOLAND hardware navigation, guidance, and control laws resident in the digital computers are described. Typical flight-test data are shown and discussed as documentation of the system performance at acceptance from the contractor.
V/Stoland Avionics System Flight-Test Data on a UH-1H Helicopter
1980
68 pages
Report
No indication
English
V/STOLAND avionics system flight-test data on a UH-1H helicopter
TIBKAT | 1980
|Helicopter avionics architecture for integrating flight critical functions
Tema Archive | 1986
|Emerald Group Publishing | 1987
|Online Contents | 2002