A True Air Speed Sensor for Miniature Unmanned Aircraft
J.A.C. Beattie
(Royal Aircraft Establishment, Farnborough, Hants, England)
62
Abstract
This paper describes the development of a laboratory prototype true air speed sensor for use on unmanned aircraft. The sensor works on vortex shedding principles and has a digital output. The vortices are sensed by thick film thermistor elements that are non‐critical in the signal circuitry.
Citation
Beattie, J.A.C. (1982), "A True Air Speed Sensor for Miniature Unmanned Aircraft", Microelectronics International, Vol. 1 No. 1, pp. 44-45. https://doi.org/10.1108/eb044114
Publisher
:MCB UP Ltd
Copyright © 1982, MCB UP Limited