A scheme to provide redundant sensor data in an automatic control system using the principle of functional redundancy is described. This scheme replaces one of three altimeters with a data processing scheme based on a Kalman filter. The filter is driven by altitude rate and acceleration signals from the air data computer and vertical accelerometer. A special initialisation technique employs the two altimeter signals. The feasibility of this scheme is indicated by tests in which data obtained from these several sensors during flight tests are used to drive the functionally redundant altimeter.
A functionally redundant altimeter
Ein funktional redundanter Hoehenmesser
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 4 ; 459-463
1976
5 Seiten, 9 Quellen
Aufsatz (Zeitschrift)
Englisch