Airspeed estimation system

Patent metadata

Field	Value
Publication number	US-10338090-B2
Application number	US-201515508413-A
Country	US
Kind code	B2
Filing date	Sep 4, 2015
Priority date	Sep 4, 2014
Publication date	Jul 2, 2019
Grant date	Jul 2, 2019

Abstract

An airspeed estimation system of an aircraft includes an electronic airspeed rate modeler unit configured to output an estimated airspeed rate signal indicating an estimated airspeed rate of the aircraft. The estimated airspeed rate signal is based on a longitudinal body acceleration of the aircraft and at least one adaptive parametric airspeed model. The airspeed estimation system further includes an electronic airspeed estimator unit in signal communication with the airspeed rate modeler unit. The airspeed estimator unit is configured to determine an estimated airspeed of the aircraft based on the estimated airspeed rate signal.

First claim

What is claimed is:

1. An airspeed estimation system of an aircraft, comprising:
a non-transitory memory having computer readable instructions;
a processor configured to execute the computer readable instructions;
an electronic airspeed rate modeler unit coupled to the processor, the electronic airspeed rate modeler unit configured to output an estimated airspeed rate signal indicating an estimated airspeed rate of the aircraft based on a longitudinal body acceleration of the aircraft and at least one adaptive parametric airspeed model; and
an electronic airspeed estimator unit coupled to the processor and in signal communication with the airspeed rate modeler unit, the airspeed estimator unit configured to:
determine an estimated airspeed of the aircraft based on the estimated airspeed rate signal;
monitor a real airspeed of the aircraft, and selectively output a first airspeed signal based on the real airspeed and a second airspeed signal based on the estimated airspeed;
wherein the first airspeed signal is output in response to the real airspeed being at least equal to the speed threshold and the second airspeed signal is output in response to the real airspeed being less than the speed threshold; and

wherein a flight control system is operable to control flight operations of the aircraft using the first airspeed signal or the second airspeed signal.

2. The airspeed estimation system of claim 1 , wherein the airspeed estimator unit determines the estimated airspeed in response to integrating the estimated airspeed rate.

3. The airspeed estimation system of claim 1 , further comprising a longitudinal body acceleration filter unit that receives a longitudinal body acceleration signal indicating the longitudinal body acceleration and outputs a filtered longitudinal body acceleration signal in response to removing at least one of gravity parameters and centrifugal force parameters from the longitudinal body acceleration signal.

4. The airspeed estimation system of claim 3 , wherein the electronic airspeed rate modeler unit further comprises a summer that determines an airspeed differential value between the filtered longitudinal body acceleration signal and the real airspeed, and applies the airspeed differential value to at least one adaptive parametric airspeed model to determine the estimated airspeed rate.

5. The airspeed estimation system of claim 4 , further comprising an electronic airspeed resynchronization unit that determines an error value between the estimated airspeed and the real airspeed, and resynchronizes the estimated airspeed with respect to the real airspeed based on a comparison between the error value and an error threshold value.

6. The airspeed estimation system of claim 5 , wherein the electronic airspeed resynchronization unit resynchronizes the estimated airspeed in response to the error value exceeding the error threshold value.

7. A method of estimating airspeed of an aircraft, the method comprising:
outputting an estimated airspeed rate signal via an electronic airspeed rate modeler unit to indicate an estimated airspeed rate of the aircraft based on a longitudinal body acceleration of the aircraft and at least one adaptive parametric airspeed model;
determining an estimated airspeed of the aircraft via an electronic airspeed estimator unit in response to integrating the estimated airspeed rate signal; and
monitoring, by the electronic airspeed estimator unit, a real airspeed of the aircraft, and selectively outputting a first airspeed signal based on the real airspeed and a second airspeed signal based on the estimated airspeed;
wherein the first airspeed signal is output in response to the real airspeed being at least equal to the speed threshold and the second airspeed signal is output in response to the real airspeed being less than the speed threshold; and
wherein a flight control system controls flight operations of the aircraft using the first airspeed signal or the second airspeed signal.

8. The method of claim 7 , further comprising measuring the longitudinal body acceleration of the aircraft and outputting a filtered longitudinal body acceleration signal in response to removing at least one of gravity parameters and centrifugal force parameters from the longitudinal body acceleration signal.

9. The method of claim 8 , further comprising determining an airspeed differential value between the filtered longitudinal body acceleration signal and the real airspeed, and determining the estimated airspeed rate in response to applying the airspeed differential value to at least one adaptive parametric airspeed model.

10. The method of claim 7 , further comprising determining an error value between the estimated airspeed and the real airspeed, and resynchronizing the estimated airspeed with respect to the real airspeed in response to the error value exceeding an error threshold value.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Bailey Jr Dale R
• Rivera Antonio

Classifications

• G01P5/02

  by measuring forces exerted by the fluid on solid bodies, e.g. anemometer · CPC title

• B64C13/503

  Fly-by-Wire · CPC title

• G01P15/00

  Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title

• G01P5/00 Primary

  Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft (application of speed-measuring devices for measuring volume of fluid G01F) · CPC title