Procedure to minimize the risk of air collision for personal mid-air vehicles
First Claim
1. A flight control system for a personal air vehicle to be flown by a person at altitudes below general aviation traffic without the assistance of air traffic controllers, which comprises:
- an altitude sensor;
a heading sensor;
a processor coupled to said altitude sensor and said heading sensor, said processor being programmed with personal air vehicle flight control rules to fly said personal air vehicle at altitudes below general aviation traffic without the assistance of air traffic controllers, said flight control rules including a minimum forward flight altitude selected to substantially avoid ground objects and a maximum forward flight altitude selected to substantially be below general aviation traffic, said flight control rules further requiring, in order to avoid a collision with other personal air vehicles, a change in altitude of the personal vehicle if there is a heading change of the personal vehicle and a reduction in airspeed of the personal vehicle if a heading change of the personal vehicle is greater than a pre-determined heading change; and
,a display coupled to said processor.
1 Assignment
0 Petitions
Accused Products
Abstract
A method of and a system for controlling personal air vehicle (PAV) traffic provides a take-off-and-landing zone, and a forward flight zone. The take-off-and-landing zone may be from the ground up to a first altitude. The forward flight zone may be from the first altitude up to a second altitude. A maximum airspeed is provided in the take-off-and-landing zone. Minimum and maximum airspeeds are provided in the forward flight zone. In the forward flight zone there is a single heading for each altitude. Any change in heading must be accompanied by a change in altitude.
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Citations
15 Claims
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1. A flight control system for a personal air vehicle to be flown by a person at altitudes below general aviation traffic without the assistance of air traffic controllers, which comprises:
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an altitude sensor; a heading sensor; a processor coupled to said altitude sensor and said heading sensor, said processor being programmed with personal air vehicle flight control rules to fly said personal air vehicle at altitudes below general aviation traffic without the assistance of air traffic controllers, said flight control rules including a minimum forward flight altitude selected to substantially avoid ground objects and a maximum forward flight altitude selected to substantially be below general aviation traffic, said flight control rules further requiring, in order to avoid a collision with other personal air vehicles, a change in altitude of the personal vehicle if there is a heading change of the personal vehicle and a reduction in airspeed of the personal vehicle if a heading change of the personal vehicle is greater than a pre-determined heading change; and
,a display coupled to said processor. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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Specification