초록 ▼

An apparatus and method for detecting the type of Selective Availability (SA) engine in a Global Positioning System (GPS) receiver. The apparatus reverse computes a User Equivalent Range Error (UERE) value and filters it. The filtered value is run through a hysteresis to determine the GPS engine ty

An apparatus and method for detecting the type of Selective Availability (SA) engine in a Global Positioning System (GPS) receiver. The apparatus reverse computes a User Equivalent Range Error (UERE) value and filters it. The filtered value is run through a hysteresis to determine the GPS engine type. The engine type determination is used to adjust values used by other systems.

대표청구항 ▼

What is claimed is: 1. An apparatus for automatically determining a Selective Availability (SA) engine type of a Global Positioning System (GPS) receiver, the apparatus comprising: a GPS receiver configured to receive signals from at least one GPS satellite, the receiver having a SA engine configur

What is claimed is: 1. An apparatus for automatically determining a Selective Availability (SA) engine type of a Global Positioning System (GPS) receiver, the apparatus comprising: a GPS receiver configured to receive signals from at least one GPS satellite, the receiver having a SA engine configured to set at least one value based on a predefined SA engine type; and a detector configured to determine the SA type of the SA engine based on a Horizontal FIG. of Merit (HFOM) value and a Horizontal Dilution of Precision (HDOP) value received from the GPS receiver, wherein the detector comprises: a first component configured to compute an estimate of User Equivalent Range Error (UERE) based on the HFOM and the HDOP values; a second component configured to filter the UFRE estimate; and a third component configured to determine the SA engine type based on the filtered UERE, wherein the receiver and detector are mounted in an aircraft. 2. The apparatus of claim 1, further comprising a component configured to set at least one value based on the engine type determination, wherein the at least one value includes a Horizontal Figure of Merit (HFOM) limit. 3. The apparatus of claim 1, wherein the second component filters based on a hysteresis analysis. 4. A method for automatically determining a selective availability engine type of a Global Positioning System (GPS) receiver, the method comprising: a) receiving signals from a GPS receiver having a selective availability engine; b) determining the type of the selective availability engine based on the received signals; c) adjusting at least one value based on the engine type determination; and d) receiving at least one Horizontal Figure of Merit (HFOM) value and at least one Horizontal Dilution of Precision (HDOP) value from the GPS receiver, wherein determining further comprises: computing an estimate of User Equivalent Range Error (UERE) based on the HFOM and the HDOP values; filtering the UERE estimate; and determining the engine type based on the filtered UERE, wherein a)-d) performed in an aircraft. 5. The method of claim 4, wherein the at least one value includes a horizontal figure of merit (HFOM) limit. 6. The method of claim 4, wherein filtering includes a hysteresis analysis. 7. The method of claim 4, wherein filtering includes a hysteresis analysis. 8. An apparatus for automatically determining a selective availability engine type of a Global Positioning System (GPS) receiver, the apparatus comprising: a means for receiving signals from a GPS receiver having a selective availability engine; a means for determining the type of the selective availability engine based on the received signals; a means for adjusting at least one value based on the engine type determination; and a means for receiving at least one Horizontal Figure of Merit (HFOM) value and at least one Horizontal Dilution of Precision (HDOP) value from the GPS receiver, wherein determining further comprises: a means for computing an estimate of User Equivalent Range Error (UERE) based on the HFOM and the HDOP values; a means for filtering the UERE estimate; and a means for determining the selective availability engine type based on the filtered UERE, wherein the means for receiver and the means for determining are mounted in an aircraft. 9. The apparatus of claim 8, wherein the means for filtering includes a hysteresis analysis. 10. The apparatus of claim 8, wherein the at least one value includes a Horizontal Figure of Merit (HFOM) limit. 11. The apparatus of claim 8, wherein the means for filtering includes a hysteresis analysis.