Path capture forcing function generator for aircraft vertical ax

Details Path capture forcing function generator for aircraft vertical ax Path capture forcing function generator for aircraft vertical ax

1989-12-15

1992-05-26

Black, Thomas G.

Boots, shoes, and leggings

244181, 244186, B64C 1318, G05D 106

Patent

active

051173620

ABSTRACT:
A path capture forcing function generator utilizes integrations from an initial altitude rate error signal and an initial altitude error signal to provide an altitude rate signal and an altitude signal which are compared to the altitude rate error and altitude error signals to provide path rate error and path error signals to the autopilot. In the process of providing the altitude rate and altitude error signals an altitude acceleration signal is established which is used as a feed forward predictor for expected normal acceleration of the aircraft.

REFERENCES:
patent: 4377848 (1983-03-01), Flannigan et al.
patent: 4413320 (1983-11-01), Brandau et al.
patent: 4709336 (1987-11-01), Zweifel
patent: 4862372 (1989-08-01), Appleford

Affiliated with

Also associated with

Rating

Path capture forcing function generator for aircraft vertical ax does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Path capture forcing function generator for aircraft vertical ax, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Path capture forcing function generator for aircraft vertical ax will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-424457