AIRCRAFT LANDING SYSTEM USING RELATIVE GNSS

• US 20110231038A1
• Filed: 03/17/2010
• Published: 09/22/2011
• Est. Priority Date: 03/17/2010
• Status: Abandoned Application

• Current Assignee: CMC Electronics Incorporated (Transdigm Group Incorporated)
• Original Assignee: CMC Electronics Incorporated (Transdigm Group Incorporated)
• Inventors: STUDENNY, John, Domey, Daniel
• Application Number:
  US12/725,948
• Publication Number:
  US 20110231038A1
• Time in Patent Office: Days
• US Class Current: 701/17
• CPC Class Codes: B64D 45/04 Landing aids; Safety measures to prevent collision with earth's surface
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]

Abstract

A method for confirming mobile base station integrity in a relative GNSS aircraft landing system, the method comprising: determining a relative position of a first GNSS antenna fixed to the mobile base station with respect to a second GNSS antenna also fixed to the mobile base station by processing signals from a GNSS satellite constellation; calculating a distance between the first GNSS antenna and the second GNSS antenna using the measured relative position; comparing a calculated distance to a known fixed distance; and confirming mobile base station integrity if the calculated distance is within a predetermined threshold of the known fixed distance.

Claims

1. An aircraft landing system comprising:

at least two mobile base station GNSS antennae at known fixed distances for receiving signals from a GNSS satellite constellation;

a mobile base station module operatively connected to the at least two mobile base station GNSS antennae and adapted to receive GNSS signals from the at least two GNSS antennae, extract measurement data therefrom, and determine relative positions of the GNSS antennae for specifying an approach path with respect to the relative positions of the mobile base station GNSS antennae, the mobile base station module also adapted to calculate a measured distance between the at least two mobile base station GNSS antennae using the relative positions and compare the measured distance with the known fixed distance to determine mobile base station integrity; and

a data transmitter for transmitting to an aircraft mobile base station integrity data, approach path data, and GNSS measurement data for at least one of the at least two mobile base station GNSS antennae.

2. The aircraft landing system of claim 1, further comprising:

an air GNSS antenna for receiving signals from the GNSS satellite constellation;

an air data receiver for receiving the mobile base station integrity data, the approach path data, and the measurement data; and

an air module connected to the data receiver and to the air GNSS antenna and adapted to extract and validate satellite data from the GNSS satellite constellation signals, determine a relative position of the air GNSS antenna to the at least one of the at least two mobile base station antennae using the extracted satellite data, the mobile base station measurement data, and the mobile base station integrity data, and determine approach guidance for the aircraft using the relative position of the air GNSS antenna to the at least one of the at least two mobile base station antennae and the approach path data.

3. The aircraft landing system of claim 2, further comprising at least two air antennae located at known and fixed distances on the aircraft for augmenting airborne integrity in a manner substantially similar to the mobile base station module.

4. The aircraft landing system of claim 2, wherein the air GNSS antenna, the data receiver, and the air module are also on the mobile base station connected to the mobile base station module and act as a closed loop verification for data transmitted by the data transmitter.

5. The aircraft landing system of claim 2, further comprising:

a set of mobile base station sensors providing data to the mobile base station;

an air data receiver adapted to decode the sensor data; and

an air module adapted to transmit the sensor data to one or more aircraft equipment.

6. The aircraft landing system of claim 5, wherein at least one of the sensors is adapted to accept operator messages for transmission to the air module.

7. The aircraft landing system of claim 1, wherein the at least two mobile base station GNSS antennae, the mobile base station module, and the data transmitter are portable for rapid deployment.

8. The aircraft landing system of claim 1, wherein the mobile base station module comprises:

a first landing system mobile base station unit having at least one of the at least two mobile base station GNSS antennae attached thereto; and

a second landing system mobile base station unit having another of the at least two mobile base station GNSS antennae attached thereto.

9. The aircraft landing system of claim 8, wherein the mobile base station module comprises a mobile base station computer operatively connected between the first landing system mobile base station unit, the second landing system mobile base station unit, and the data transmitter, the mobile base station computer adapted to calculate the distance between the at least two mobile base station GNSS antennae and compare the measured distance with the known and fixed distance.

10. The aircraft landing system of claim 1, wherein the mobile base station module comprises:

a landing system mobile base station unit having more than one of the at least two mobile base station GNSS antennae attached thereto; and

a mobile base station computer adapted to calculate the distance between the mobile base station GNSS antennae and compare the measured distance with the known and fixed distance.

11. The aircraft landing system of claim 1, wherein the data transmitter is adapted to modulate data for transmission onto a Radio Frequency (RF) signal and transmit the RF signal.

12. The aircraft landing system of claim 7, wherein the air module is adapted to transmit data to at least one aircraft equipment.

13. The aircraft landing system of claim 2, wherein the air module may selectively be set for relative GNSS use and Ground-Based Augmentation System (GBAS) use and the air data receiver is adapted to receive both RGNSS and GBAS data.

14. The aircraft landing system of claim 13, wherein the air module may also selectively be set for Spaced-Based Augmentation System (SBAS) use.

15. A method for confirming mobile base station integrity in a relative GNSS aircraft landing system, the method comprising:

determining a relative position of a first GNSS antenna fixed to the mobile base station with respect to a second GNSS antenna also fixed to the mobile base station by processing signals from a GNSS satellite constellation;

calculating a distance between the first GNSS antenna and the second GNSS antenna using the measured relative position;

comparing a calculated distance to a known fixed distance; and

confirming mobile base station integrity if the calculated distance is within a predetermined threshold of the known fixed distance.

16. The method of claim 15, further comprising transmitting a mobile base station integrity confirmation to an aircraft.

17. The method of claim 16, wherein transmitting mobile base station integrity data comprises transmitting a result of a comparison of the distance between the first fixed GNSS antenna and the second fixed GNSS antenna with respect to the threshold and any available satellite specific integrity information.

18. The method of claim 16, wherein transmitting mobile base station integrity comprises modulating integrity data onto an RF signal and transmitting the RF signal.

19. The method of claim 15, wherein determining a relative position of the two fixed GNSS antennae comprises measuring the position of a first fixed GNSS antenna by receiving signals through the first antenna from the GNSS satellite constellation, extracting data from the satellite signals, and calculating the position of the first fixed GNSS antenna based on measurements of the satellite signals;

and measuring the position of a second fixed GNSS antenna by receiving signals through the second antenna from the GNSS satellite constellation, extracting data from the satellite signals, and calculating the position of the second fixed GNSS antenna based on measurements of the satellite signals; and

computing an offset between the two measured positions to obtain the relative position.

20. The method of claim 15, wherein determining a relative position of the two fixed GNSS antennae comprises receiving signals through the first antenna from the GNSS satellite constellation, extracting data from the satellite signals, and making measurements of the satellite signals;

and receiving signals through the second antenna from the GNSS satellite constellation, extracting data from the satellite signals, and making measurements of the satellite signals; and

calculating the relative position of the two GNSS antenna based on a combination of both sets of measurements of the satellite signals taken from each antenna.

21. The method of claim 15, further comprising receiving the signals from the GNSS satellite constellation using at least two GNSS antennae, wherein the measured distance between several pairs, of GNSS antenna are compared to their known fixed distances;

and confirming mobile base station integrity if the calculated distances are within a predetermined threshold of the known fixed distances.

22. The method of claim 15, wherein a difference between the known fixed relative position of the two GNSS antennae and the measured relative position is compared with predetermined difference thresholds to confirm mobile base station integrity.

23. A method for aircraft approach and landing using relative GNSS positioning, the method comprising:

determining relative positions of at least two mobile base station GNSS antennae provided at a known fixed distance;

determining an approach path relative to the at least two mobile base station GNSS antennae;

confirming mobile base station integrity by comparing a measured distance between the mobile base station GNSS antennae with the known fixed distance;

transmitting to an aircraft the mobile base station integrity data, approach path data, and satellite measurement data for one of the at least two mobile base station GNSS antennae;

receiving the mobile base station integrity data, the approach path data, and the satellite measurement data at the aircraft;

determining a relative position with integrity of an air GNSS antenna on the aircraft with respect to one of the at least two mobile base station GNSS antennae using combined satellite measurements from the air antenna and the mobile base station antenna; and

determining approach guidance using the relative position of the air and mobile base station GNSS antennae and the approach path data.

24. The method of claim 23, wherein determining an approach path comprises:

using one of the at least two mobile base station GNSS antennae as an approach end point;

using another of the at least two mobile base station GNSS antennae to trace a vector between the at least two mobile base station GNSS antennae;

applying a translation and rotation to the vector appropriate to a local environment; and

expressing the approach path as a path relative to the position of one of the at least two mobile base station GNSS antenna.

25. The method of claim 23, wherein determining approach guidance comprises using the relative position of the air GNSS antenna with respect to one of the at least two mobile base station GNSS antennae in combination with the approach path data relative to a same mobile base station GNSS antenna in a way to cancel any common mode errors in the satellite measurements to the air and mobile base station antennae.

26. The method of claim 23, wherein determining relative position with integrity comprises computing the relative position in a way to cancel any common mode errors in the satellite measurements to the air and mobile base station antennae, and using integrity data transmitted from a mobile base station.

27. The method of claim 23, further comprising enhancing integrity by applying a Fault Detection Error algorithm to a position solution.

28. The method of claim 23, further comprising enhancing integrity by applying base station sensor data to a position solution.