http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2014047578-A1

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_81936aa8d69f2b3ff3feb015e1e1b75b
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D43-02
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http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S19-40
filingDate 2013-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ea2ef685a1584dbfc597c16650ffd909
publicationDate 2014-03-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber WO-2014047578-A1
titleOfInvention Determination and tracking of centripetal acceleration and acceleration-based velocity
abstract The flight of an aircraft is represented in terms of Earth-based reference system data for a first position and a second position of the aircraft that are separated by a time increment. A centripetal acceleration of the aircraft is determined based on the Earth-based reference system data for the positions in conjunction with the time increment. A rate of rotation is established corresponding to the time increment in an aircraft-based reference system. Aircraft airspeed is determined based on the centripetal acceleration and the rate of rotation. A turn can be detected by a change in track angle from a prior GPS packet compared to a new packet. Aircraft turns can be detected based on a change in track angle in GPS packets. Compensation can be applied to a gyro based on centripetal acceleration such that the gyro more accurately responds to the Earth gravity axis.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106406355-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106406355-A
priorityDate 2012-09-21-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 23.