Method and apparatus for determining aircraft bank angle based on satellite navigational signals

• US 5,451,963 A
• Filed: 05/26/1994
• Issued: 09/19/1995
• Est. Priority Date: 05/26/1994
• Status: Expired due to Term

• Current Assignee: Sodo US LLC (Intellectual Ventures LLC)
• Original Assignee: Thomas A. Lempicke
• Inventors: Lempicke, Thomas A.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/249,803
• Time in Patent Office: 481 Days
• Field of Search: 342/357, 364/434, 364/441, 364/447
• US Class Current: 342/357.31
• CPC Class Codes: G01S 11/10 using Doppler effect
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

An apparatus for determining the bank angle of a moving aircraft includes a receiver for receiving navigational signals from NAVSTAR/GPS satellites in orbit about the earth, a signal processor for demodulating the satellite navigational signals, an arrangement for determining aircraft speed based on the navigational signals, an arrangement for determining the rate of change of the aircraft track heading from the navigational signals, an arrangement for determining the bank angle of the moving aircraft from the aircraft speed and the rate of change of track heading wherein the aircraft bank angle is inversely proportional to the aircraft speed and directly proportional to the rate of change of track heading.

Claims

1. An apparatus for determining the bank angle of a moving aircraft comprising:

receiver means for receiving navigational signals from satellites in orbit about the earth;

signal processing means for demodulating the satellite navigational signals;

means for determining aircraft speed based on said navigational signals;

means for determining the rate of change of the aircraft track heading from said navigational signals; and

means for determining the bank angle of the aircraft from said aircraft speed and said rate change in track heading wherein said bank angle is inversely proportional to said aircraft speed and directly proportional to said rate of change in track heading.

2. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said receiver means includes at least one antenna for receiving positional signals from said satellites.

3. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said speed determining means, said beading change rate determining means and said bank angle determining means are preprogrammed microprocessors receiving input from said signal processing means.

4. An apparatus for determining the bank angle of a moving aircraft according to claim 3 and further comprising means for displaying said bank angle determined by said determining means in a pilot readable manner.

5. An apparatus for determining the bank angle of a moving aircraft according to claim 4 wherein said display means includes housing means configured to mount said device in an aircraft control panel.

6. An apparatus for determining the bank angle of a moving aircraft according to claim 4 wherein said display means includes a portable, hand held housing.

7. An apparatus for determining the bank angle of a moving aircraft according to claim 3 wherein the aircraft includes an automatic piloting system and said bank angle determining means is operatively connected to the automatic piloting system includes means for operationally applying the determined bank angle to the automatic piloting system.

8. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said receiver means and said signal processing means are disposed in a preexisting, hand held, commercially available satellite navigational receiver having a housing and a display screen, and said speed determining means, said heading change rate determining means and bank angle determining means are disposed within said housing and are operatively connected to said receiver means, signal processing means and display screen for using said hand held receiver in a moving aircraft to display the bank angle thereof.

9. An apparatus for determining the bank angle of a moving aircraft according to claim 8 wherein said speed determining means, said heading change rate determining means and said bank angle determining means are preprogrammed microprocessors receiving input from said signal processing means.

10. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said navigational signals include a clock signal and said signal processing means includes means to define a first aircraft position and a second aircraft position different from said first aircraft position and said means for determining aircraft speed includes means for calculating aircraft speed based on the distance between said first aircraft position and said second aircraft position and the time of traversal of said distance, said traversal time being determined from said clock signal.

11. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said signal processing means includes means for determining the Doppler shift in satellite carrier frequency and said means for determining aircraft speed includes a microprocessor preprogrammed with information to include the fixed velocity of the satellites and means to relate the Doppler shift of the satellite carrier frequency with the satellite velocity to determine an effective Doppler shift in satellite carrier frequency which is proportional to aircraft speed.

12. An apparatus for determining the bank angle of a moving aircraft according to claim 1 wherein said navigational signals include a clock signal and said means for determining rate of change of aircraft track heading includes means for predicting the straight line displacement of the aircraft after a predetermined time period based .on the aircraft heading and means for determining the actual displacement of the aircraft after said predetermined time period, means for determining the deviation of actual displacement from predicted displacement per unit time as measured by said clock signal thereby determining the rate of change of the aircraft track heading.

13. A method for determining the bank angle of a moving aircraft comprising the steps of:

receiving navigational signals from satellites in orbit about the earth;

processing said navigational signals;

determining aircraft speed based on said processed signals;

determining the rate of change of the aircraft track heading from said navigational signals;

determining the bank angle of the aircraft from said aircraft speed and said rate of change of aircraft track heading; and

displaying the aircraft bank angle in a pilot readable manner.

14. A method for determining the bank angle of a moving aircraft according to claim 13 wherein the step of determining aircraft bank angle includes determining said bank angle as being inversely proportional to said aircraft speed and directly proportional to said rate of change of track heading.