A gyro-less wing leveler and directional autopilot were developed and flight tested in a single-engine light airplane. The primary purpose of the project was to develop a simple, reliable, low-cost stability augmentation and autopilot system for light aircraft. The wing leveler used a fluidic inertial rate sensor, electronic signal processing circuitry, and vacuum operated servos. A strap-down magnetic heading reference of simple design provided the wing leveler with directional autopilot capability. Flight tests indicated that the performance of the gyro-less wing leveler was equal to that of a commercial wing leveler using a gyroscopic rate sensor. Drift-free, long-term, heading-hold capability of the magnetic heading reference was demonstrated. (Author)
Development and Flight Tests of a Gyro-Less Wing Leveler and Directional Autopilot
1974
53 pages
Report
Keine Angabe
Englisch
Development Of Maneuvering Autopilot For Flight Tests
NTRS | 1992
|Development of a 'Gyro-Less' Digital Flight Director
NTIS | 1972
|