IP Library Granted Patent US 10,416,310
Granted Patent B2
US 10,416,310 · App. 12/138,722 · Granted Sep 17, 2019

Integrated positioning solution for global navigation satellite systems

Inventors: Michael Kirchner (Munich, DE); Tanja Rang (Grasbrunn, DE); Hans L. Trautenberg (Ottobrunn, DE)
Assignee: AIRBUS DEFENCE AND SPACE GMBH
G01S19/02G01S19/05G01S19/08G01S19/33B64G1/36
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Quick Facts
Patent No.
US 10,416,310
App. No.
12/138,722
Granted
Sep 17, 2019
Kind
B2
Abstract

The invention includes a process for one's own global navigation satellite system and at least one other global navigation satellite system including the following: Receiving ranging signals and navigation messages or ranging signals only from the at least one other global navigation satellite system, and processing the received ranging signals and navigation messages in a similar way as the ranging signals and navigation messages of the owned global navigation satellite system.

Claims (18)

1. A process for an own global navigation satellite system and at least one other global navigation satellite system, said process comprising:

receiving ranging signals including only encrypted navigation data or no navigation data from the at least one other global navigation satellite system;

processing the received ranging signals from the at least one other global navigation satellite system in a manner similar to the processing of navigation messages from ranging signals of the own global navigation satellite system to compute navigation messages for the at least one other global navigation satellite system for users of the own global navigation satellite system; and

transmitting the computed navigation messages of the at least one other global navigation satellite system from satellites of the own global navigation satellite system.

2. A process according to claim 1 , further comprising:

up-loading the computed navigation messages of the at least one other global navigation satellite system to respective satellites of the own global navigation satellite system;

wherein the transmitting comprises disseminating, by the respective satellites, the up-loaded computed navigation messages of the at least one other global navigation satellite system to user receivers of the own global navigation satellite system.

3. A system comprising an own global navigation satellite system and at least one other global navigation satellite system, said system comprising:

a receiver structured and arranged for receiving ranging signals including only encrypted navigation data or no navigation data from the at least one other global navigation satellite system;

a processor structured and arranged for processing the received ranging signals from the at least one other global satellite system in a manner similar to the processing of the received ranging signals into navigation messages of the own global navigation satellite system to compute navigation messages for the at least one other global navigation satellite system; and

a transmitter structured and arranged for transmitting the computed navigation messages of the at least one other global navigation satellite system from satellites of the own global navigation satellite system.

4. A system according to claim 3 , further comprising:

an up-load link structured and arranged for up-loading the computed navigation messages of the at least one other global navigation satellite system to the satellites of the own global navigation satellite system;

wherein the transmitter is further structured and arranged for disseminating the up-loaded computed navigation messages of the at least one other global navigation satellite system to user receivers of the own global navigation satellite system.

5. An apparatus of a global navigation satellite system comprising:

a receiver structured and arranged for receiving ranging signals including only encrypted navigation data or no navigation data from at least one global navigation satellite system other than an own global navigation satellite system;

a processor structured and arranged for processing the received ranging signals from the at least one global navigation satellite system other than an own global navigation satellite system in a manner corresponding to that in which ranging signals of the owned global navigation satellite system are processed into navigation messages of the own global navigation satellite system, thereby computing navigation messages of the at least one global navigation satellite system other than the own global navigation satellite system; and

an up-load link structured and arranged for up-loading the computed navigation messages of the at least one global navigation satellite system other than the own global navigation satellite system to the respective satellites of the own global navigation satellite system.

Assignments (3)
MERGER Recorded Jan 10, 2019
From: AIRBUS DS GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 048043/0373 →
CHANGE OF NAME Recorded Oct 30, 2018
From: ASTRIUM GMBH
To: AIRBUS DS GMBH
Reel/Frame 047906/0600 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 13, 2008
From: KIRCHNER, MICHAEL; RANG, TANJA; TRAUTENBERG, DR. HANS L
To: ASTRIUM GMBH
Reel/Frame 021830/0128 →
Priority Claims (1)
EP 07011582 · Jun 13, 2007 · regional
Continuity (1)
Related Publication 20090322602A1 · Dec 31, 2009