A general theory of the design of flight vehide instruments and sensors is developed, and methods of calculating their static and dynamic characteristics, instrument errors, and reliability reartings are prosented. A general method for calculating the characteristics and errors of instruments and sensors, based on an analysis of structural circuits, is presented. This method gives a clear idea of the role of transforming elements in the formation of the resulting characteristics and errors of instruments and sensors.
Flight vehicle instruments and senscrs
Titel russisch
1970
1 Seite, 154 Quellen
Article (Journal)
Russian
Online Contents | 1994
Engineering Index Backfile | 1920
|Experimental Flight Instruments
NTIS | 1967
|Flight instruments & automatic flight control systems
TIBKAT | 2004
|Engineering Index Backfile | 1930