Glider aircraft tow control system

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

114246, 244135A, B64C 3702, B64D 300, B64D 3900

Patent

active

051883139

ABSTRACT:
The towed glider flight control system of the invention has a towing frame interconnecting and pivotally connected at each end to the towed glider and the towing aircraft. Sensors measuring the angular relationships between the towing frame and the towed glider and the rage of change in these relationships and sensors measuring flight conditions of the glider and towing aircraft are connected to the input of a computer of which the output connects to the glider aerodynamic control surface. The computer determines differences between sensor sensed parameter values existing when a selected spatial geometric relationship exists between the glider and towing aircraft and sensor parameter values received by the computer from the sensors and from these differences the computer calculates motions required of the glider aerodynamic flight path control surfaces to establish a glider flight which establish and maintain the selected spatial geometric relationship of the glider and towing aircraft.

REFERENCES:
patent: 2385392 (1945-09-01), Van Dusen
patent: 2476301 (1949-07-01), Jenks
patent: 4014481 (1977-03-01), Daikeler et al.
patent: 4674710 (1987-06-01), Rodriguez
McKenzie, WO88/05395, Pub S.R. Jul. 28, 1988.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Glider aircraft tow control system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Glider aircraft tow control system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Glider aircraft tow control system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2199588

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.