In-flight transceiver and locator system
First Claim
1. An in-flight transceiver system for communicating an information securely at a high data rate between an in-flight unit and a ground unit comprising:
- an antenna;
an aviation box conforming to a one-half, half short Air Transport Rack (ATR) form factor comprising a transceiver and a global positioning system (GPS) unit;
a switch between the aviation box and the antenna for controlling a data signal between the antenna and the transceiver, andan interface comprising a servicing data connector and an in-flight data connector coupled to the in-flight unit wherein connecting a cable to the servicing data connector automatically disables the in-flight data connector,wherein the transceiver operates at a data rate of greater than approximately 800 bits per second (bps) when sending information from the in-flight unit to the ground unit and greater than approximately 2800 bps when receiving information at the in-flight unit from the ground unit, andwherein the information from the in-flight unit to the ground unit and the information from the ground unit to the in-flight unit is packet encrypted using a Triple Data Encryption Standard (DES) algorithm and an Advanced Encryption Standard (AES) algorithm, or a DES algorithm and a Rivest Shamir Adleman (RSA) algorithm, or an AES algorithm and an RSA algorithm.
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Accused Products
Abstract
Military systems in particular face two specific problems: field casualties typically increase as unit visibility decreases and it is often difficult for ground stations and/or headquarters to maintain control and visibility of geographically dispersed assets. The system provides satellite communications such as two-way messaging, Voice over Packet, and global positioning information and reporting for fixed and rotary wing aircrafts where traditional methods of communications are not otherwise practical. The system provides communications between remote users and other remote users as well as between remote users and control stations. In some embodiments there is an in-flight transceiver system that includes an antenna, an aviation box, and a switch. The aviation box conforms to a one-half, ½ short Air Transport Rack (ATR) form factor and includes a transceiver, an interface card, and a global positioning system (GPS) unit. The switch is located between the aviation box and the antenna for controlling a data signal between the antenna and the transceiver of the aviation box.
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Citations
30 Claims
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1. An in-flight transceiver system for communicating an information securely at a high data rate between an in-flight unit and a ground unit comprising:
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an antenna; an aviation box conforming to a one-half, half short Air Transport Rack (ATR) form factor comprising a transceiver and a global positioning system (GPS) unit; a switch between the aviation box and the antenna for controlling a data signal between the antenna and the transceiver, and an interface comprising a servicing data connector and an in-flight data connector coupled to the in-flight unit wherein connecting a cable to the servicing data connector automatically disables the in-flight data connector, wherein the transceiver operates at a data rate of greater than approximately 800 bits per second (bps) when sending information from the in-flight unit to the ground unit and greater than approximately 2800 bps when receiving information at the in-flight unit from the ground unit, and wherein the information from the in-flight unit to the ground unit and the information from the ground unit to the in-flight unit is packet encrypted using a Triple Data Encryption Standard (DES) algorithm and an Advanced Encryption Standard (AES) algorithm, or a DES algorithm and a Rivest Shamir Adleman (RSA) algorithm, or an AES algorithm and an RSA algorithm. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
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19. A method for securely communicating between a first party and a second party comprising:
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providing to the second party an in-flight transceiver system comprising; an antenna; an aviation box conforming to a one-half, half short Air Transport Rack (ATR) form factor comprising a transceiver and a global positioning system (GPS) unit; a switch between the aviation box and the antenna for controlling a data signal between the antenna and the transceiver; and an interface comprising a servicing data connector and an in-flight data connector coupled to the in-flight transceiver wherein connecting a cable to the servicing data connector automatically disables the in-flight data connector; sending a first independent communications packet over a first communications channel that is not allocated or predetermined; and sending a second independent communications packet over a second communications channel before receiving acknowledgement of successful receipt of the first communications packet, wherein the first and second communications packets are sent between the first and second party, wherein the transceiver operates at a data rate of greater than approximately 800 bits per second (bps) when sending the first or second independent communications packet from the second party to the first party and greater than approximately 2800 bps when receiving the first or second independent communications packet at the second party from the first party, and wherein at least one of the first or second communications packets is packet encrypted using a Triple Data Encryption Standard (DES) algorithm and an Advanced Encryption Standard (AES) algorithm, or a DES algorithm and a Rivest Shamir Adleman (RSA) algorithm, or an AES algorithm and an RSA algorithm. - View Dependent Claims (20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30)
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Specification