Landing assistance system using navigation satellites

• US 4,894,655 A
• Filed: 02/26/1988
• Issued: 01/16/1990
• Est. Priority Date: 02/27/1987
• Status: Expired due to Fees

• Current Assignee: LMT Radio Professionnelle
• Original Assignee: LMT Radio Professionnelle
• Inventors: Joguet, Jean C., Schilliger, Michel
• Primary Examiner(s): Orsino, Joseph A.
• Assistant Examiner(s): Swarthout, Brent A.
• Application Number:
  US07/161,099
• Time in Patent Office: 690 Days
• Field of Search: 340/988, 340/993, 340/989, 340/947, 340/952, 340/945, 342/352, 342/356, 342/357, 342/358, 342/408, 364/439, 364/444, 364/449, 364/460, 364/424
• US Class Current: 340/988
• CPC Class Codes: G01S 1/56 Timing the pulse-type envelope signals derived by reception of the beam
• CPC Class Codes: G01S 19/07 providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

The system according to the invention uses GPS/NAVSTAR navigation satellites and includes:

a fixed station located in the vicinity of the landing zone, containing a receiver for positioning by satellite that gives an estimate of the position of this fixed station and computing means that give correction data representing the deviation between this estimate and a reference position; and a data transmitter transmitting, in particular, these correction data on a radio channel which is conventionally used to transmit data in a microwave landing system called the MLS system;

an on-board station in each aircraft comprising: an MLS receiver capable of receiving the ancillary data transmitted by the MLS system, a receiver for positioning by satellite and a computing device by which the correction data can be used to correct an estimate of position given by the positioning receiver.

Claims

1. A landing assistance system using navigation satellites, said system comprising several navigation satellites emitting signals controlled by a clock, a fixed station located in the vicinity of landing strips, said fixed station comprising:

a receiver for positioning by satellite, said receiver giving an estimate of the position of said fixed station, and computing means giving correction data representing the deviation between this estimate and a reference position;

radio transmission means transmitting in a radio channel according to the standards of the microwave landing system known as MLS, to transmit correction data, and landing data associated with each landing strip respectively, including the magnetic alignment, the coordinates of the approach, end of the landing strip and the identity of the landing strip;

said system further comprising a station on-board each aircraft, said on-board station comprising;

a conventional radio receiver to receive data transmitted by a microwave landing system known as MLS;

a receiver for positioning by satellite, and computing means that give an estimate of the position of the aircraft, corrected by means of the correction data received by the radio receiver.

2. A landing assistance system according to claim 1 wherein the fixed station receiver for positioning by satellite consists of a conventional receiver for non-differential positioning by satellite, the estimate of the position of the fixed station given by the positioning receiver consisting of an estimate of the three geodesic coordinates of the fixed station,

and wherein the correction data essentially consist of the deviations between this estimate and reference values, and of numbers identifying the satellites, the transmissions of which have been used to estimate the position of the fixed station;

and wherein each on-board station'"'"'s receiver for positioning by satellite comprises a conventional receiver for non-differential positioning by satellite, the corrected estimate of the position of the on-board station consisting of a corrected estimate of the three geodesic coordinates of the on-board station, using transmissions of satellites designated by the numbers transmitted by the fixed station and using correction data transmitted by the fixed station in the radio channel according to the MLS landing system.

3. A landing assistance system according to claim 1 wherein the estimate of the position of the fixed station, given by the fixed station receiver for positioning by satellite, comprises an estimate of the pseudo-distances between the fixed station and each of the system'"'"'s satellites, the transmissions of which can be received by the fixed station, the correction data essentially comprising the deviations between this estimate and the values computed from the reference values;

and wherein the receiver for positioning by satellite and the computing means of each on-board station comprise a conventional receiver for differential positioning by satellite;

the corrected estimate of the position of the on-board station being made by an estimate of the pseudo-distances between the on-board station and several satellites respectively, the transmissions of which can be received by the on-board station, the estimate of these pseudo-distances beeing corrected by means of correction data transmitted by this fixed station on a radio channel according to the standards of the MLS landing system.

4. A landing assistance system according to claim 1 wherein the radio transmission means further transmit data proper to the landing zone, especially the coordinates of the approch end of a landing strip, these coordinates having been measured, in a reference point of the fixed station, by means of a station placed on board an aircraft positioned on this approach end.