Tail tracking antenna
An unmanned aerial vehicle (UAV) and a system of communication between an unmanned aerial vehicle with a ground controller, the UAV having a top side, a bottom side, and an antenna side. The antenna side of the UAV can have a hinge to which a flat panel antenna can be disposed is pivotably coupled. The flat panel antenna can be actively controlled or passively controlled by gravity.
1. An unmanned aerial vehicle, comprising:
a hinge, coupled to the unmanned aerial vehicle; and
a housing;
a flat panel antenna disposed within the housing and is pivotably coupled to the hinge to change a pitch of the flat panel antenna; and
wherein the flat panel antenna is freely pivotably coupled to the hinge and is actuated by a force of gravity.
2. The unmanned aerial vehicle of claim 1 further comprising an actuator to actively control the pitch the flat panel antenna.
3. The antenna device of claim 2 , wherein the actuator is a servo motor.
4. The unmanned aerial vehicle of claim 1 , further comprising a gap sufficiently spaced between the flat panel antenna and the housing to create an air resistance to dampen a free pivoting movement of the flat panel antenna by said force of gravity, and a size of the gap remains consistent as the panel antenna freely and hysteretically pivots by said force of gravity.
5. The unmanned aerial vehicle of claim 1 , wherein the housing has a bottom wall, said bottom wall has an arcuate shape.
6. The unmanned aerial vehicle of claim 1 , wherein the housing is airtight.
7. The antenna device of claim 1 , wherein the housing comprises:
a first wall coupled to the hinge;
the first wall is arranged to stop the flat antenna on the first wall when the unmanned aerial vehicle tilts more than a first angle, wherein the first angle is at most 55 degrees to a vertical axis perpendicular to the hinge.
8. The antenna device of claim 7 , wherein the housing further comprises:
a second wall coupled to the hinge;
the second wall is arranged to stop the flat antenna on the second wall when the unmanned aerial vehicle tilts more than a second angle, wherein the second angle is at most −55 degrees to a vertical axis perpendicular to the hinge.
9. A UAV (unmanned aerial vehicle) communication system, comprising:
a UAV having a top side, bottom side, and an antenna side;
a ground controller configured to send a positional information of the ground controller to the UAV causing the UAV to constantly remain facing the ground controller with the antenna side, regardless of a relative orientation of the UAV to the ground controller;
an antenna device coupled to the antenna side of the UAV, the antenna device comprising:
a hinge coupled to the unmanned aerial vehicle; and
a flat panel antenna pivotably coupled on the hinge.
10. The communication system of claim 9 further comprising an actuator to actively control a pitch the flat panel antenna, wherein the actuator is one selected from the group consisting of a servo motor, and a gimbal.
11. The communication system of claim 9 , wherein the antenna device further comprises a housing to enclose the flat panel antenna, and the flat panel antenna pivots relative to the housing.
12. The communication system of claim 11 , wherein the flat panel antenna is freely pivotably coupled to the hinge and is actuated by a force of gravity.
13. The communication system of claim 12 further comprising a gap sufficiently spaced between the flat panel antenna and the housing to create an air resistance to dampen a free pivoting movement of the flat panel antenna by said force of gravity, and a size of the gap remains consistent as the panel antenna freely and hysteretically pivots by said force of gravity.
14. The communication system of claim 12 , wherein the housing has a bottom wall, said bottom wall has an arcuate shape.
15. The communication system of claim 12 , wherein the housing comprises:
a first wall coupled to the hinge;
wherein the first wall is arranged to stop the flat antenna on the first wall when the unmanned aerial vehicle tilts more than a first angle, wherein the first angle is at most 55 degrees to a vertical axis perpendicular to the hinge.
16. The communication system of claim 15 , wherein the housing further comprises:
a second wall coupled to the hinge;
wherein the second wall is arranged to stop the flat antenna on the second wall when the unmanned aerial vehicle tilts more than a second angle, wherein the second angle is at most −55 degrees to a vertical axis perpendicular to the hinge.