Aircraft location and tracking system

• US 20020173888A1
• Filed: 01/07/2002
• Published: 11/21/2002
• Est. Priority Date: 05/21/2001
• Status: Abandoned Application

• Current Assignee: Demetrius Ramone Ross, Lewis Ruff Dodds, Robert Leo Shelton
• Original Assignee: Demetrius Ramone Ross, Lewis Ruff Dodds, Robert Leo Shelton
• Inventors: Shelton, Robert Leo, Dodds, Lewis Ruff, Ross, Demetrius Ramone
• Application Number:
  US10/037,880
• Publication Number:
  US 20020173888A1
• Time in Patent Office: Days
• US Class Current: 701/35
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

An integrated flight safety apparatus containing a 12-channel GPS (Global Positioning System) receiver that networks a flight data recorder to a satellite communications system. This device is capable of providing real-time data acquisition and analysis to a ground-based monitoring and tracking station. The aircraft location and tracking system extracts data from any data collection device by utilizing serial port to serial port communications. A call is established from the tracking station to the apparatus, then the extracted data is polled to the base station at user defined intervals over the satellite link. Simultaneously, the aircraft'"'"'s location is displayed on a moving aerial map in relation to its global position. In addition, different aerial maps, airspace mapping, waypoints, airports and runway approaches may be downloaded and displayed on the user'"'"'s monitor and tracked on the remote monitor. This device utilizes voice command technology and can also be used as a satellite telephone device.

Claims

1. An integrated flight apparatus for networking a flight data recorder or data collection system to a multifunctional GPS receiver and satellite communication tracking device comprising:

An integrated microprocessor incorporating on board RAM (Random Access Memory), buffers and EEPROM (Electrically erasable programmable read-only memory). The processor or CPU (Central Processing Unit) is attached to the circuit board via the data and system busses. These circuits connect every component on the circuit board providing bi-directional communication between component devices. The CPU is responsible for processing data from the satellite transceiver, GPS receiver, LCD (Liquid Crystal Display) screen and any other data that can be inputted and outputted through the serial ports;

Multiple serial ports (Four) with alternate protocol specifications such as RS-232 and Parallel/SCSI (Small Computer Serial Interface). The serial ports that are attached to the processor via the circuit board for data and signal exchange;

ROM (Read-only memory) microchips are linked to the processor via the system and data bus that provides operational system pre-programmed functions and calculations;

2. The integrated GPS device recited in claim 1, containing an embedded modem (Modulator/demodulator), that is used to convert analog signals to digital signals, and vice-versa, digital signals to analog signals, by the process of modulation and demodulation. All computer-based electronics and equipment communicate digitally on the same circuit board or remotely with each other, but is generally transmitted over an analog frequency connecting the devices. The modem accommodates the two distinct frequencies and translates between them. Quite often, telephone companies and (ISP'"'"'s) Internet Service Providers transmit data over an analog signal.

3. The integrated GPS device recited in claim 1, comprising a rugged external covering completely encased around the apparatus, suitably built to meet the requirements of mounted aircraft equipment approved by the (FAA) Federal Aviation Administration.

4. The integrated GPS device recited in claim 1, claiming no electronics embodied in the flight apparatus interfere with the normal operation of an aircraft or any other electronic device on an aircraft, according to FAA equipment requirements.

5. The integrated GPS device recited in claim 3, where at least one of the serial ports attached to the flight apparatus meet RS-232 connection specification standards.

6. The integrated GPS device recited in claim 1, where the flight apparatus draws its primary power from the aircraft'"'"'s existing electrical system.

7. The integrated GPS device recited in claim 1, where the flight apparatus includes a serial port connection that can be directly interfaced with a serial port on a flight data recorder for transporting data.

8. The integrated GPS device recited in claim 1, where the integrated processor includes an EEPROM smart chip.

9. The integrated GPS device recited in claim 8, comprising a software driver that oversees the control parameters of hardware'"'"'s functionality between the data ports of the flight apparatus and the flight data recorder.

10. The integrated GPS device recited in claim 9, comprising an integrated oscillator that is responsible for generating all system clocking parameters (Timing) for the processor, modem and all other circuit board components.

11. The integrated GPS device recited in claim 8, where the processor is unified in one integrated microchip.

12. The integrated GPS device recited in claim 11, where the processor computes and executes software during normal operation and is capable of software storage, even in the absence of power.

13. The integrated GPS device recited in claim 8, comprising four serial connectors attached to the flight apparatus to interface the flight data recorder and other alternative flight system data collectors.

14. The integrated GPS device recited in claim 1, where the integrated processor includes nonvolatile flash memory for saving and storing downloaded programs that are executed by the processor.

15. The integrated GPS device recited in claim 1, comprising a built in condenser microphone (MIC) on the flight apparatus for capturing and relaying all audio input. The mic is able to send voice transmissions and understand voice commands.

16. The integrated GPS device recited in claim 1, comprising a built-in speaker system on the flight apparatus that is responsible for delivering sound to the user.

17. An interface device for interfacing a flight data recorder with a GPS receiver and tracking device, a satellite transceiver and providing real-time data analysis to a display screen and ground-based monitoring station, comprising:

A processor linked to the serial port for processing data from the flight data recorder and the GPS receiver for bi-directional communications with the satellite transceiver, including;

A power supply conditioning unit linked to the system components and for providing predetermined electrical characteristics for signals transmitted to and received from the interface device. Also, supplying a means for stabilizing DC voltage to the flight apparatus system components,

An integrated GPS 12-channel receiver capable of triangulating global position on an aerial moving map and forwarding that information via modem and satellite transceiver to a ground-based tracking and monitoring station,

An integrated satellite transceiver capable of providing satellite communications over a high-speed satellite network. Polling of data is initialized from the ground-based monitoring station at user defined intervals. This transceiver can bi-directionally carry voice, data and video.