Method of detecting erroneous GPS ground speed on ground
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G01C-023/00
출원번호
US-0426547
(2006-06-26)
등록번호
US-8271191
(2012-09-18)
발명자
/ 주소
Ishihara, Yasuo
Conner, Kevin J
Johnson, Steve C.
출원인 / 주소
Honeywell International Inc.
대리인 / 주소
Lowe Graham Jones PLLC
인용정보
피인용 횟수 :
0인용 특허 :
14
초록▼
Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GP
Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed. The system sets a GPS ground speed based on the determined reliability. A GPS ground speed output is set to zero, if the GPS ground speed is determined unreliable and the GPS ground speed output is set to the GPS ground speed, if the GPS ground speed is determined reliable. The system sends the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). Also, the system sets the GPS ground speed output to zero, if a received GPS ground speed validity signal or a received GPS track validity signal indicate invalid.
대표청구항▼
1. A method for determining reliability of Global Positioning System (GPS) ground speed, the method comprising: at a processing device, receiving GPS track information and GPS ground speed;determining a change in GPS track information over a predefined time delay;determining reliability of the GPS g
1. A method for determining reliability of Global Positioning System (GPS) ground speed, the method comprising: at a processing device, receiving GPS track information and GPS ground speed;determining a change in GPS track information over a predefined time delay;determining reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed,wherein the GPS ground speed is determined reliable if the change in GPS track information does not differ by more than a threshold amount, wherein the threshold amount is based on the GPS ground speed;setting a GPS ground speed based on the determined reliability; andsetting the GPS ground speed output to zero, if the GPS ground speed is determined unreliable. 2. The method of claim 1, further comprising setting the GPS ground speed output to the GPS ground speed, if the GPS ground speed is determined reliable. 3. The method of claim 2, further comprising sending the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). 4. The method of claim 2, further comprising sending the GPS ground speed output to an Enhanced Ground Proximity Warning System. 5. The method of claim 2, further comprising: receiving at least one of a GPS ground speed validity signal and a GPS track validity signal; andsetting the GPS ground speed output to zero, if at least one of the GPS ground speed validity signal or the GPS track validity signal indicates invalid. 6. The method of claim 5, further comprising sending the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). 7. A system for determining reliability of Global Positioning System (GPS) ground speed, the system comprising: a first means for receiving GPS track information and GPS ground speed;a second means for determining a change in GPS track information over a predefined time delay;a third means for determining reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed,wherein the GPS ground speed is determined reliable if the change in GPS track information does not differ by more than a threshold amount, wherein the threshold amount is based on the GPS ground speed; anda fourth means for setting a GPS ground speed based on the determined reliability, the fourth means sets the GPS ground speed output to zero, if the GPS ground speed is determined unreliable. 8. The system of claim 7, wherein the fourth means sets the GPS ground speed output to the GPS ground speed, if the GPS ground speed is determined reliable. 9. The system of claim 8, further comprising a fifth means for sending the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). 10. The system of claim 9, further comprising: a fifth means for receiving at least one of a GPS ground speed validity signal and a GPS track validity signal,wherein the fourth means sets the GPS ground speed output to zero, if one of the GPS ground speed validity signal or the GPS track validity signal indicates invalid. 11. The system of claim 10, further comprising a sixth means for sending the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). 12. The system of claim 7, wherein the first, second, and third means are included in a Runway Awareness and Advisory System (RAAS). 13. The system of claim 7, wherein the first, second, and third means are included in an Enhanced Ground Proximity Warning System.
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이 특허에 인용된 특허 (14)
McIntyre, Melville Duncan W., Apparatus and method for navigation of an aircraft.
Conner, Kevin J; Gremmert, Scott R.; Ishihara, Yasuo; Khatwa, Ratan; Poe, John J.; Corcoran, III, James J., Ground operations and imminent landing runway selection.
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