H. Hartmann

In general, the term "monitoring system" comprises the two elements "observing" and "recording the observation". This paper focuses on a monitoring within the primary control loop of a future flight control system. In addition to low critical simplex monitoring systems, the described class of safety-critical redundant monitoring systems also take a specific action following a failure and thereby affect the observed units, i.e. they are reconfiguring the control system. These monitoring systems induce fault-tolerance to the control loop and recursively these monitoring systems themselves are invulnerable to any effects of any causes of arbitrary failures. The basic structure of such a monitoring concept is sketched.

DGLR Symposium, Stuttgart, 1995

Conference Paper

englisch

17,0 x 24 cm, 23 Seiten

DGLR-Bericht, 1995, 1995-03, Aircraft Integrated Monitoring Systems; S.621-643; 1995; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

monitoring

Bestellbar

1995