Adaptive aircraft actuator fault detection

Details Adaptive aircraft actuator fault detection Adaptive aircraft actuator fault detection

1980-08-26

1982-10-19

Smith, Jerry

Boots, shoes, and leggings

244 1713, 244195, 364150, 364151, G06F 1550, G06G 778

Patent

active

043553583

ABSTRACT:
The operation of an actuator (16) is monitored by comparing its position (21) with the position (31, 136) indicated by a model which integrates (45, 135) a limited amount of the difference between the position command (24) applied to the actuator and the achieved model position (31, 136), the limited amount being variable (63, 67, 124) from a nominal limit (61, 65, 124) in dependence upon limited functions (74, 90, 114, 116) of the difference (33, 109) between the actuator position and the model position, and additionally reduced (80, 94, 122) when pilot input overrides (50, 108) the position of the actuator.

REFERENCES:
patent: 4148452 (1979-04-01), Niessen et al.
patent: 4206891 (1980-06-01), Perez et al.
patent: 4213175 (1980-07-01), Kurihara
patent: 4249238 (1981-02-01), Spang et al.

Affiliated with

Also associated with

Rating

Adaptive aircraft actuator fault detection does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Adaptive aircraft actuator fault detection, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Adaptive aircraft actuator fault detection will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1341088