ProceedingsIEEE, 1990 - Avionics |
Contents
A Fault Tolerant Fly By Wire System | 11 |
Dynamic Model Dependency for a Decentralized | 47 |
Pole Placement | 64 |
Copyright | |
38 other sections not shown
Common terms and phrases
activity addition aircraft algorithm allow analysis application approach architecture associated automated automatic avionics changes commands communication complex components configuration consists contains cost defined dependency described detection determine devices display distributed document effects elements engine environment error evaluation example execution failure fault tolerance Figure flight frequency functions given hardware implementation increase initial input integrated interface launch limited measurement memory method mission mode modules monitoring navigation node object operation output performance phase pilot position possible presented problem processor production receiver reduce redundancy reference reliability requirements Research response selected sensor shown signal simulation single space specification speed standard structure subsystem Table task techniques testability tion units validation vehicle