Method and system for providing aeronautical communication services
First Claim
1. Apparatus for an aircraft in a first aeronautical communication system to allow communication to and from a land-based station, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a mobile satellite service system, the apparatus comprising:
- a transmitting unit configured to transmit communications from the aircraft to the land-based station using the first low frequency band, wherein the first low frequency band is an L-band and a fuselage of the aircraft shields transmission of the communications according to the first low frequency band to the land-based station from interference from an orbiting satellite receiving other transmissions from the land-based station using the first low frequency band; and
a receiving unit configured to receive communications from the land-based station using the second low frequency band, the second low frequency band is distinct from the first low frequency band.
1 Assignment
0 Petitions
Accused Products
Abstract
Aeronautical communication services is disclosed. For example, an aeronautical vehicle for use in a first aeronautical communication system to allow communication to and from a land-based station is disclosed, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a second aeronautical communication system. In the first aeronautical communication system, the aeronautical vehicle transmits communications using the first low frequency band and receives communications using the second low frequency band.
-
Citations
19 Claims
-
1. Apparatus for an aircraft in a first aeronautical communication system to allow communication to and from a land-based station, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a mobile satellite service system, the apparatus comprising:
-
a transmitting unit configured to transmit communications from the aircraft to the land-based station using the first low frequency band, wherein the first low frequency band is an L-band and a fuselage of the aircraft shields transmission of the communications according to the first low frequency band to the land-based station from interference from an orbiting satellite receiving other transmissions from the land-based station using the first low frequency band; and a receiving unit configured to receive communications from the land-based station using the second low frequency band, the second low frequency band is distinct from the first low frequency band. - View Dependent Claims (2, 3)
-
-
4. Apparatus for a flying vehicle with fixed wings to allow aeronautical communication to and from a land-based station, comprising:
-
a transmitting unit configured to transmit communications from the flying vehicle with fixed wings to the land-based station using a frequency band of a L-band; and a receiving unit configured to receive communications from the land-based station using a frequency band of a S-band, wherein a fuselage of the flying vehicle shields the communications from the land-based station from interference from transmissions from an orbiting satellite transmitting in the S-band. - View Dependent Claims (5, 6)
-
-
7. A powered flying vehicle with fixed wings for use in a first aeronautical communication system to allow communication to and from a land-based station, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a second aeronautical communication system, the second aeronautical communication system is a mobile satellite service system, the powered flying vehicle with fixed wings comprising:
-
a transmitting unit configured to transmit communications from the powered flying vehicle with fixed wings to the land-based station using the first low frequency band, wherein the first low frequency band is an L-band and a fuselage of the powered flying vehicle mitigates interference from transmissions from the land-based station to an orbiting satellite using the first low frequency band; and a receiving unit configured to receive communications from the land-based station using the second low frequency band, the second low frequency band is distinct from the first low frequency band and is an S-band. - View Dependent Claims (8, 9)
-
-
10. A method for use in an aeronautical vehicle that sustains powered flight through a fixed wing and thrust from a gas turbine engine in a first aeronautical communication system to allow communication to and from a land-based station, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a second aeronautical communication system, the method comprising:
-
transmitting communications from the aeronautical vehicle to the land-based station using the first low frequency band; receiving communications from the land-based station using the second low frequency band, wherein the first low frequency band is an L-band, the second low frequency band is an S-band; and shielding, by a fuselage of the aeronautical vehicle, reception of the communications from the land-based station and transmission of the communications to the land-based station from interference from transmissions from an orbiting satellite that transmits or receives signals using the first low frequency band or the second low frequency band. - View Dependent Claims (11)
-
-
12. A processor for an aeronautical vehicle in a first aeronautical communication system to control communication to and from a land-based station, wherein the land-based station transmits communications using a first low frequency band and receives communications using a second low frequency band in accordance with a second aeronautical communication system and wherein an aerodynamic force acting on an airfoil associated with the aeronautical vehicle sustains continuous flight of the aeronautical vehicle, the processor configured to control:
-
transmission of communications to the land-based station from the aeronautical vehicle using the first low frequency band, wherein the transmission of the communications to the land-based station are shielded from interference from an orbiting satellite receiving communications from the land-based station using the first low frequency band by a fuselage of the aeronautical vehicle; and reception of communications from the land-based station to the aeronautical vehicle using the second low frequency band, wherein the first low frequency band is an L-band frequency band and the second low frequency band is an S-band frequency band. - View Dependent Claims (13, 14)
-
-
15. An aeronautical vehicle for allowing aeronautical communication to and from a land-based station, wherein the aeronautical vehicle achieves powered flight through use of an airfoil and an associated gas-turbine engine;
- the aeronautical vehicle comprising;
a transmitting unit configured to transmit communications from the aeronautical vehicle to the land-based station using a frequency band of an L-band, wherein the communications from the aeronautical vehicle to the land-based station are shielded from communication interference from an orbiting satellite receiving communications in the L-band by a body section of the aeronautical vehicle; and a receiving unit configured to receive communications from the land-based station to the aeronautical vehicle using a frequency band of an S-band. - View Dependent Claims (16, 17)
- the aeronautical vehicle comprising;
-
18. A method for use in an aeronautical vehicle to allow aeronautical communication to and from a land-based station, comprising:
-
transmitting communications to the land-based station from the aeronautical vehicle using a frequency band of an L-band; receiving communications from the land-based station to the aeronautical vehicle using a frequency band of an S-band; and protecting, with a body section of the powered flying vehicle, the communications from the land-based station to the aeronautical vehicle using the S-band and the communications from the aeronautical vehicle to the land-based station using the L-band from interference from an orbiting satellite transmitting in the S-band and from the land-based station transmitting in the L-band, wherein the aeronautical vehicle is a powered flying vehicle with fixed wings.
-
-
19. An aeronautical vehicular system allowing aeronautical communication to and from a land-based station, comprising:
-
means for transmitting communications to the land-based station from a powered flying vehicle with fixed wings using a frequency band of an L-band; and means for receiving communications from the land-based station to the aeronautical vehicle using a frequency band of an S-band; and means for protecting, with a body section of the powered flying vehicle, the communications from the land-based station to the aeronautical vehicle using the S-band and the communications from the aeronautical vehicle to the land-based station using the L-band from interference from an orbiting satellite transmitting in the S-band and from the land-based station transmitting in the L-band.
-
Specification