Automatic approach to hover system

Details Automatic approach to hover system Automatic approach to hover system

G - Physics

05

D

343/22, 343/79,

G05D 1/00 (2006.01) G05D 1/10 (2006.01)

Patent

CA 1081830

ABSTRACT OF THE DISCLOSURE In a helicopter having an automatic pilot system for controlling the main rotor collective pitch, main rotor longitudinal and lateral cyclic pitch, and tail rotor collective pitch, in response to inputs provided from normal sensors, navigational instruments and controls, (which include a among others is known, doppler radar, a pilot panel, an air speed indicator, a radar altimeter. a barometric altimeter and a longitudinal accelerometer). commands to control automatic approach to a desired hover position are provided to the autopilot system in response to signals normally supplied by a TACNAV unit as well as the sensors, navigational units and controls; controls are provided for altitude and rate of descent, so as to terminate in hover at a desired altitude, as well as for turns, courses, and speed so as to approach the desired point of hover upwind and to decelerate in a controlled fashion to hover.

271669

Affiliated with

Also associated with

Rating

Automatic approach to hover 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 Automatic approach to hover system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Automatic approach to hover system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-631303