Method and apparatus for determining a calibrated value for the yaw angle of a satellite

• US 6,804,986 B2
• Filed: 05/02/2001
• Issued: 10/19/2004
• Est. Priority Date: 11/06/1998
• Status: Expired due to Fees

• Current Assignee: SES ASTRA SA (SES SA)
• Original Assignee: SES ASTRA SA (SES SA)
• Inventors: Patouraux, Christian
• Primary Examiner(s): OEN, WILLIAM L
• Application Number:
  US09/847,268
• Publication Number:
  US 20020116993A1
• Time in Patent Office: 1,266 Days
• Field of Search: 73/17.8, 73/17.5, 73/17.6, 73/17.7, 731/78.R
• US Class Current: 73/1.78
• CPC Class Codes: B64G 1/244 Spacecraft control systems
• CPC Class Codes: B64G 1/245 Attitude control algorithms for spacecraft attitude control
• CPC Class Codes: B64G 1/285 using momentum wheels
• CPC Class Codes: B64G 1/365 using horizon or Earth sensors
• CPC Class Codes: B64G 1/369 using gyroscopes as attitude sensors
• CPC Class Codes: G01C 21/24 specially adapted for cosmonautical navigation

Abstract

The method according to the invention allows to determine the yaw angle of a satellite from the reading of two different sensors measuring the roll and/or pitch angles, provided that the reference point of the two sensors are not identical. A description is given basically for geostationary satellites but the method can be applied directly to satellites which are stationary with respect to any star. The method can be employed for circular and non-circular orbits.

Claims

1. Method for determining a calibrated value for a yaw angle of a satellite, comprising the steps of:

storing a yaw angle profile over a quiet orbit,

determining a sample yaw angle at a calibration time (t0),

determining a calibrated value by subtracting the sample yaw angle with a yaw angle profile value having a time shift in the yaw angle profile corresponding to the calibration time (t0).

2. Method for determining a calibrated value for a yaw angle of a satellite having angle sensors on board, comprising:

storing for each of the angle sensors on board the satellite a profile over a quiet orbit,

determining a sample value for each of the angle sensors at a calibration time (t0), determining calibrated values for each of the angle sensors by subtracting the sample values with an angle sensor profile value having a time shift in the respective angle sensor profile corresponding to the calibration time (t0), and

determining a calibrated value for a yaw angle with calibrated values for each of the angle sensors.

3. Apparatus for determining a calibrated value for a yaw angle of a satellite, comprising:

means for storing a yaw angle profile over a quiet orbit,

means for determining a sample yaw angle at a calibration time (t0),

means for determining a calibrated value by subtracting the sample yaw angle with a yaw angle profile value having a time shift in the yaw angle profile corresponding to the calibration time (t0).

4. Apparatus for determining a calibrated value for a yaw angle of a satellite having angle sensors on board comprising:

means for storing for each of the angle sensors on board the satellite a profile over a quiet orbit,

means for determining a sample value for each of the angle sensors at a calibration time (t0),

means for determining calibrated values for each of the angle sensors by subtracting the sample values with an angle sensor profile value having a time shift in the respective angle sensor profile corresponding to the calibration time (t0), and

means for determining a calibrated value for a yaw angle with calibrated values for each of the angle sensors.