Dynamic effective isotropic radiated power spectral density control

• US 10,320,471 B1
• Filed: 06/26/2018
• Issued: 06/11/2019
• Est. Priority Date: 06/26/2018
• Status: Active Grant

• Current Assignee: Panasonic Avionics Corporation (Panasonic Holdings Corporation)
• Original Assignee: Panasonic Avionics Corporation (Panasonic Holdings Corporation)
• Inventors: Panthi, Sunil, McLain, Christopher
• Primary Examiner(s): Trinh, Tan H
• Application Number:
  US16/019,433
• Time in Patent Office: 350 Days
• Field of Search: 455 121, 455427, 455 131, 455 134, 455522, 455430, 455509, 370316, 343879
• CPC Class Codes: H04B 7/18508 with satellite system used as relay, i.e. aeronautical mobile satellite service
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18543 for adaptation of transmission parameters, e.g. power control for detecting or preventing errors in the information received H04L1/00
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

An aeronautical satellite broadband communications system has an antenna defined by a transmit gain pattern varying according to an orientation relative to a geostationary orbit satellite. An antenna controller unit is connected to an aircraft inertial navigation system and receptive to navigation data therefrom, and a set of antenna orientation data is derived from the navigation data on a real-time basis. A broadband controller connected to the antenna controller unit generates a set of output variables as a function of normalized equivalent isotropic radiated power spectral density values of the antenna and the set of antenna orientation data. The set of output variables controls the output power and carrier bandwidth of transmissions from the antenna within predefined limits of equivalent isotropic radiated power spectral density that vary with values of the set of antenna orientation data.

Claims

1. An aeronautical satellite broadband communications system, comprising:

an antenna defined by a transmit gain pattern varying according to an orientation relative to a geostationary orbit satellite;

an antenna controller unit connected to an aircraft inertial navigation system and receptive to navigation data therefrom, a set of antenna orientation data being derived from the navigation data on a real-time basis;

a broadband controller connected to the antenna controller unit, and generating a set of output variables as a function of normalized equivalent isotropic radiated power spectral density values of the antenna derived from the transmit gain pattern and the set of antenna orientation data, the set of output variables controlling output power and carrier bandwidth of transmissions from the antenna within predefined limits of equivalent isotropic radiated power spectral density varying with values of the set of antenna orientation data; and

a satellite modem connected to the antenna and to the broadband controller, the output power and carrier bandwidth of the satellite modem to the antenna being set based upon the output variables from the broadband controller.

2. The system of claim 1, wherein the predefined limits of the output power and the carrier bandwidth is based upon a regulatory compliance mask applied to the normalized equivalent isotropic radiated power spectral density values.

3. The system of claim 2, wherein the regulatory compliance mask includes a mask opening defined by off-axis angle limits of the orientation of the antenna to the geostationary orbit satellite.

4. The system of claim 2, wherein the regulatory compliance mask is offset proportionally to all off-axis angles of the orientation of the antenna to the geostationary orbit satellite.

5. The system of claim 1, wherein the navigation data is selected from a group consisting of:

aircraft location, aircraft roll angle, aircraft pitch angle, and aircraft heading.

6. The system of claim 1, wherein the orientation of the antenna relative to the geostationary orbit satellite is selected from a group consisting of:

skew angle, elevation angle, and azimuthal angle.

7. The system of claim 1, wherein the output variables is selected from a group consisting of:

saturated power, reference power, and reference bandwidth.

8. The system of claim 1, wherein the satellite modem operates in a login state with transmissions generated during the login state having a predefined fixed bandwidth and the output power corresponding to the set of output variables from the broadband controller.

9. The system of claim 1, wherein the satellite modem operates in an operational state with the transmissions generated during the operational state having a variable bandwidth and variable output power dependent upon data rate demands.

10. The system of claim 1, wherein the antenna is selected from a group consisting of:

an electronically steered low profile antenna, a mechanically steered high profile antenna, and a parabolic antenna.

11. A method for controlling equivalent isotropic radiated power spectral density of a communications link between an aircraft and a geosynchronous orbit satellite, the method comprising:

retrieving navigation data from an avionics bus of the aircraft;

selecting a satellite beam from a plurality of available satellite beams for establishing the communications link to the geosynchronous orbit satellite, each of the satellite beams being associated with a regulatory compliance mask;

retrieving antenna orientation data from an antenna controller unit, the antenna orientation data being derived from the navigation data and is representative of an orientation of the antenna relative to the geosynchronous orbit satellite;

generating, on a broadband controller, a set of output variables as a function of the antenna orientation data, a set of normalized equivalent isotropic radiated power spectral density values for an antenna mounted to the aircraft, and the regulatory compliance mask; and

relaying the output variables to a modem, an output power and a carrier bandwidth of the satellite beam transmitted from the antenna being controllable by the output variables for transmissions to be within predefined limits of equivalent isotropic radiated power spectral density.

12. The method of claim 11, wherein the normalized equivalent isotropic radiated power spectral density values of the antenna are precomputed from a transmit gain pattern thereof.

13. The method of claim 11, wherein the regulatory compliance mask includes a mask opening defined by off-axis angle limits of the orientation of the antenna to the geostationary orbit satellite.

14. The method of claim 11, wherein the regulatory compliance mask is offset proportionally to all off-axis angles of the orientation of the antenna to the geostationary orbit satellite.

15. The method of claim 11, wherein the predefined limits of equivalent isotropic radiated power spectral density varies in real-time according to changing orientation of the antenna relative to the geosynchronous orbit satellite during flight maneuvers of the aircraft.

16. The method of claim 11, wherein the regulatory compliance mask is specific to a geographic region in which the aircraft is flying.

17. The method of claim 11, wherein the navigation data is selected from a group consisting of:

aircraft location, aircraft roll angle, aircraft pitch angle, and aircraft heading.

18. The method of claim 11, wherein the orientation of the antenna relative to the geostationary orbit satellite is selected from a group consisting of:

skew angle, elevation angle, and azimuthal angle.

19. The method of claim 11, wherein the output variables is selected from a group consisting of:

saturated power, reference power, and reference bandwidth.

20. A non-transitory computer readable medium connectible to an aeronautical satellite broadband communications system including instructions executable by the system for performing a method of controlling equivalent isotropic radiated power spectral density of a communications link between the system and a geosynchronous orbit satellite, the method comprising:

retrieving navigation data from an avionics bus of the aircraft;

selecting a satellite beam from a plurality of available satellite beams for establishing the communications link to the geosynchronous orbit satellite, each of the satellite beams being associated with a regulatory compliance mask;

retrieving antenna orientation data from an antenna controller unit, the antenna orientation data being derived from the navigation data and is representative of an orientation of the antenna relative to the geosynchronous orbit satellite;

generating, on a broadband controller, a set of output variables as a function of the antenna orientation data, a set of normalized equivalent isotropic radiated power spectral density values for an antenna mounted to the aircraft, and the regulatory compliance mask; and

relaying the output variables to a modem, an output power and a carrier bandwidth of the satellite beam transmitted from the antenna being controllable by the output variables for transmissions to be within predefined limits of equivalent isotropic radiated power spectral density.