PAR (Position and Rate) gyro, developed by Guidance Technology, Inc, is used as single sensor for heading-hold performance and lateral mode stability in Beech KDB-1 target and Douglas A4D-1 aircraft; single degree of freedom gyro with internal electromechanical integrator provides desired yaw attitude signal for performing straight azimuth courses and senses aircraft lateral rates for Dutch roll stability augmentation; principle, examples of uses, and available designs.
Directional stability and control with single gyro
Aerospace Eng
Aerospace Engineering ; 20 , n 9
1961
3 pages
Aufsatz (Zeitschrift)
Englisch
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