1. A method for interference control, comprising:
receiving at a base station an interference report from a neighbor base station, wherein the interference report indicates interference observed at the neighbor base station; and
regulating, by the base station, data transmissions for terminals based on the interference report received from the neighbor base station, wherein regulating the data transmissions comprises identifying disadvantaged terminals and assigning the disadvantaged terminals with lower data rates, and wherein identifying a particular terminal as a disadvantaged terminal comprises comparing estimated channel gain for the terminal against a channel gain threshold.
2. The method of claim 1, wherein the disadvantaged terminals are identified in the interference report.
3. The method of claim 1, further comprising lowering a high transmit power limit that is applicable to the disadvantaged terminals.
4. The method of claim 1, further comprising lowering a lower transmit power limit that is applicable to the disadvantaged terminals.
5. A base station that is configured for interference control, comprising:
a processor;
memory in electronic communication with the processor; and
instructions stored in the memory, the instructions being executable to:
receive an interference report from a neighbor base station, wherein the interference report indicates interference observed at the neighbor base station; and
regulate data transmissions for terminals based on the interference report received from the neighbor base station, wherein regulating the data transmissions comprises identifying disadvantaged terminals and assigning the disadvantaged terminals with lower data rates, and wherein identifying a particular terminal as a disadvantaged terminal comprises comparing estimated channel gain for the terminal against a channel gain threshold.
6. The base station of claim 5, wherein the disadvantaged terminals are identified in the interference report.
7. The base station of claim 5, wherein the instructions are also executable to lower a high transmit power limit that is applicable to the disadvantaged terminals.
8. The base station of claim 5, wherein the instructions are also executable to lower a lower transmit power limit that is applicable to the disadvantaged terminals.
9. A base station that is configured for interference control, comprising:
means for receiving an interference report from a neighbor base station, wherein the interference report indicates interference observed at the neighbor base station; and
means for regulating data transmissions for terminals based on the interference report received from the neighbor base station, wherein the means for regulating the data transmissions comprises means for identifying disadvantaged terminals and means for assigning the disadvantaged terminals with lower data rates, and wherein the means for identifying a particular terminal as a disadvantaged terminal comprises means for comparing estimated channel gain for the terminal against a channel gain threshold.
10. The base station of claim 9, wherein the disadvantaged terminals are identified in the interference report.
11. The base station of claim 9, further comprising means for lowering a high transmit power limit that is applicable to the disadvantaged terminals.
12. The base station of claim 9, further comprising means for lowering a lower transmit power limit that is applicable to the disadvantaged terminals.
13. A non-transitory processor-readable storage medium, comprising:
code for receiving at a base station an interference report from a neighbor base station, wherein the interference report indicates interference observed at the neighbor base station; and
code for regulating, by the base station, data transmissions for terminals based on the interference report received from the neighbor base station, wherein the code for regulating the data transmissions comprises code for identifying disadvantaged terminals and code for assigning the disadvantaged terminals with lower data rates, and wherein the code for identifying a particular terminal as a disadvantaged terminal comprises code for comparing estimated channel gain for the terminal against a channel gain threshold.
14. The non-transitory processor-readable storage medium of claim 13, wherein the disadvantaged terminals are identified in the interference report.
15. The non-transitory processor-readable storage medium of claim 13, further comprising code for lowering a high transmit power limit that is applicable to the disadvantaged terminals.
16. The non-transitory processor-readable storage medium of claim 13, further comprising code for lowering a lower transmit power limit that is applicable to the disadvantaged terminals.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A personal aircraft comprising:
a fuselage, having a longitudinal axis and a vertical axis;
a forward wing coupled to the fuselage and located forward of a center of gravity of the aircraft;
an aft wing coupled to the fuselage and located aft of the center of gravity of the aircraft;
a port propulsion boom coupled to the fuselage and oriented substantially parallel to the longitudinal axis of the fuselage along its port side;
a port propeller coupled to the port propulsion boom for providing forward thrust;
a first plurality of rotors coupled to the port propulsion boom, the rotors of the first plurality arranged substantially parallel to the longitudinal axis of the fuselage, each rotor coupled to a motor, wherein each rotor provides thrust in a direction primarily along the vertical axis;
a starboard propulsion boom coupled to the fuselage and oriented substantially parallel to the longitudinal axis of the fuselage along its starboard side;
a starboard propeller coupled to the starboard propulsion boom for providing forward thrust;
a second plurality of rotors coupled to the starboard propulsion boom, the rotors of the second plurality arranged substantially parallel to the longitudinal axis of the fuselage, each rotor coupled to a motor, wherein each rotor provides thrust in a direction primarily along the vertical axis;
wherein each motor coupled to the plurality of rotors is adapted to be controlled independently of the other motors; and
wherein at least one of the first plurality of rotors and at least one of the second plurality of rotors is coupled in an orientation to provide a non-zero component of thrust in a direction not on the vertical axis.
2. The personal aircraft of claim 1 wherein the first plurality of rotors includes at least 4 rotors and the second plurality of rotors includes at least 4 rotors.
3. The personal aircraft of claim 1 further comprising a flight computer coupled to the fuselage and adapted to:
determine a current orientation of the personal aircraft;
determine a desired orientation of the personal aircraft; and
command independently each of the plurality of motors attached to the rotors according to a difference between the current orientation of the personal aircraft and the desired orientation of the personal aircraft.
4. The personal aircraft of claim 3, wherein the flight computer further comprises:
a position sensor interface, adapted to receive sensor data that indicates the aircraft’s position, altitude, attitude and velocity; and
a rotor control module, coupled to the position sensor interface, adapted to determine an amount of thrust required from each of the plurality of rotors to achieve the desired orientation and to command independently each of the plurality of motors to produce the determined required thrust.
5. The personal aircraft of claim 4 wherein the flight computer further comprises:
a propeller control module coupled to the position sensor interface, adapted to determine an amount of forward thrust required from each propeller and to command the propellers to produce the required thrust.
6. The flight computer of claim 4 further comprising:
a database including programmed trajectories for ascent and descent of the aircraft.
7. The personal aircraft of claim 1 wherein the port propulsion boom and the starboard propulsion boom are each coupled to the fuselage by a plurality of struts.
8. An aircraft comprising:
a fuselage;
a forward wing coupled to the fuselage and located forward of a center of gravity;
an aft wing coupled to the fuselage and located aft of the center of gravity;
a first plurality of lift rotors located between the forward wing and the aft wing on a port side of the fuselage, at least one of the first plurality having a first cant and at least one of the plurality having a second cant, the second cant having an angle different from the first cant;
a second plurality of lift rotors located between the forward wing and the aft wing on a starboard side of the fuselage, at least one of the second plurality having a third cant and at least one of the plurality having a fourth cant, the fourth cant having an angle different from the third cant;
a propeller coupled to the fuselage for providing forward thrust; and
a flight computer, coupled to the fuselage, and configured to independently control an amount of thrust provided by each of the first plurality and each of the second plurality of lift rotors.
9. The aircraft of claim 8 wherein a number of rotors in the first plurality of lift rotors is 4 and a number of rotors in the second plurality of lift rotors is 4.
10. The aircraft of claim 8 wherein a number of rotors in the first plurality of lift rotors is 3 and a number of rotors in the second plurality of lift rotors is 3.
11. The aircraft of claim 8 wherein the aft wing includes winglet features.
12. The aircraft of claim 11 wherein the winglets are oriented substantially in an upward vertical direction.
13. The aircraft of claim 11 wherein the winglets are oriented substantially in a downward vertical direction.
14. The aircraft of claim 8 wherein the lift rotors are driven by electric motors.
15. The aircraft of claim 8 wherein the forward and aft wings are not coplanar.
16. The aircraft of claim 8 wherein the wings are foldable.
17. The aircraft of claim 8 wherein an autopilot provides for unmanned operation.
18. The aircraft of claim 8 wherein the lift rotor blades have fixed pitch.
19. An aircraft comprising:
a fuselage;
a forward wing coupled to the fuselage and located forward of a center of gravity;
an aft wing coupled to the fuselage and located aft of the center of gravity;
a first mounting boom coupled to a port side of the fuselage;
a second mounting boom coupled to a starboard side of the fuselage;
a first plurality of lift rotors, each rotor mounted on the first mounting boom between the forward wing and the aft wing on the port side of the fuselage, at least one of the first plurality having a first cant and at least one of the plurality having a second cant, the first cant having an angle different from the second cant;
a second plurality of lift rotors, each rotor mounted on the second mounting boom between the forward wing and the aft wing on the starboard side of the fuselage, at least one of the second plurality having a third cant and at least one of the plurality having a fourth cant, the third cant having an angle different from the fourth cant;
a first propeller coupled to the first mounting boom for providing forward thrust;
a second propeller coupled to the second mounting boom for providing forward thrust; and
a flight computer, coupled to the fuselage, for independently controlling an amount of thrust provided by each of the first plurality and each of the second plurality of lift rotors.
20. The aircraft of claim 19 further comprising a first fence on the port side of the aircraft and a second fence on the starboard side of the aircraft, each fence essentially parallel to the mounting booms and coupled to the fuselage on an outboard side of the plurality of rotors.
21. The aircraft of claim 20 wherein the fences are adapted to reduce a noise footprint of the aircraft.