Many existing guided missiles include an autopilot whose function is to so convert steering command intelligence from a source external to the autopilot into motions of the missile's control surfaces that the resultant missile maneuver satisfies the command. An autopilot generally employs the use of feedback from the control surfaces, through the aerodynamics, as sensed by such end-instruments as accelerometers and rate gyros, and into suitable circuitry so that the experienced missile motion might be summed against that called for. This paper is concerned with a specific design for a portion of the circuitry interposed between the sensing instruments and the autopilot over-all feedback summation point.
Transistorized Operational Demodulator Driver. Design Study and Evaluation
1960
109 pages
Report
No indication
English
An Evaluation of Transistorized Ignition Systems
SAE Technical Papers | 1964
|Transistorized blocking generator
NTRS | 1974
|Service equipment with transistorized ignition
Engineering Index Backfile | 1961
|An optical transistorized ignition system
Tema Archive | 1976
|