METHOD OF AND SYSTEM FOR CALCULATION AND CONSOLIDATION OF FLIGHT PARAMETERS OF AN AIRCRAFT
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Aug 6, 2015
app pub date -
Sep 5, 2013
filing date -
Sep 5, 2012
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A method and system for calculation and consolidation of a first plurality of aircraft flight parameters including a second plurality of pressure sensors is provided. The pressure sensors are arranged in respective aircraft locations; each pressure sensor provides a pressure value based on a respective detected static pressure value. The method comprises: acquiring the pressure values from the pressure sensors; defining an equation system by associating with each pressure value a respective non-linear mathematical model describing the aerodynamic aircraft behaviour at the pressure sensor location, each respective mathematical model being a flight parameter function; iteratively solving the equation system, obtaining a current value of each of said flight parameters; calculating a plurality of intermediate pressure values by applying the current flight parameter values to each mathematical model; comparing each pressure value with the respective intermediate pressure value, obtaining a result value; and detecting an operation state of the pressure sensors.
First Claim
Family
International Classification(s)
Cited Art Landscape
Patent Citation Ranking
Advertisement
Advertisement
Advertisement
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully