Gyroless platform stabilization techniques

• US 5,124,938 A
• Filed: 07/23/1990
• Issued: 06/23/1992
• Est. Priority Date: 07/23/1990
• Status: Expired due to Fees

• Current Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Recon/Optical, Inc. (Bourns Incorporated)
• Inventors: Algrain, Marcelo C.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): AUCHTERLONIE, THOMAS
• Application Number:
  US07/557,401
• Time in Patent Office: 701 Days
• Field of Search: 364/453, 364/174, 364/559, 364/566, 318/649, 352/243, 248/550, 354/70, 354/81, 354/293
• US Class Current: 702/141
• CPC Class Codes: B64G 1/22 Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
• CPC Class Codes: B64G 1/28 using inertia or gyro effect
• CPC Class Codes: B64G 1/36 using sensors, e.g. sun-sensors, horizon sensors
• CPC Class Codes: F16F 15/02 Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems F16F15/005 takes precedence ; layered products B32B; suppression of vibration in ships B63; relieving load on bearings, using magnetic means F16C39/06
• CPC Class Codes: G01C 21/18 Stabilised platforms, e.g. by gyroscope
• CPC Class Codes: G02B 27/644 compensating for large deviations, e.g. maintaining a fixed line of sight while a vehicle on which the system is mounted changes course
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform

Abstract

A method and apparatus for platform stabilization. The apparatus uses linear and/or angular accelerometers to derive the roll, pitch, and yaw components of the angular velocity of the vehicle the apparatus is mounted on. Based on the calculation of angular velocity or acceleration of the vehicle and the current rate and angle of rotation of the device to be stabilized, the apparatus generates setpoint and movement commands for servo motors that rotate the sensing device such that the line of sight of the sensing device is stabilized. A control system implements a velocity control system, or, alternatively, an acceleration control system. In one embodiment of the invention, the accelerometers are positioned on a mounting base along axes corresponding to the roll, pitch and yaw axes of the vehicle in a location adjacent to the sensing device. In an alternative embodiment, the accelerometers are positioned on the stabilized element itself, with the command strategy being to force gimbal rotations so that the output of the accelerometers is urged towards a null value.

Claims

1. Apparatus for stabilizing an object around at least first and second object axes of rotation with respect to an inertial frame of reference, said object being carried by a vehicle subjected to rotational movement around at least first and second vehicle axes of rotation corresponding to said at least first and second object axes of rotation, said apparatus comprising in combination:

means for generating vehicle rotation signals corresponding to the rotational movement of said vehicle around at least said first and second vehicle axes of rotation with respect to said inertial frame of reference;

feedback means for generating feedback signals corresponding to the movement of said object around at least said first and second object axes of rotation independent of said inertial frame of reference;

control system means responsive to said vehicle rotation signals and responsive to said feedback signals for generating movement signals; and

movement means responsive to said movement signals for rotatably moving said object around at least said first and second object axes, whereby said object is stabilized around at least said first and second object axes with respect to said frame of reference without the use of a gyroscope as said vehicle undergoes rotation relative to said inertial frame of reference.

2. Apparatus, as claimed in claim 1, wherein said vehicle rotation signals comprise vehicle rotational velocity signals corresponding to the rotational velocities of said vehicle around at least said first and second vehicle axes of rotation.

3. Apparatus, as claimed in claim 2, wherein said means for generating comprises:

linear accelerometer means carried by said vehicle independent of said object for generating linear acceleration signals corresponding to the linear accelerations of said vehicle; and

processor means for calculating said rotational velocity signals in response to said linear acceleration signals.

4. Apparatus, as claimed in claim 1, wherein said vehicle rotation signals comprises vehicle rotational acceleration signals corresponding to the rotational accelerations of said vehicle around at least said first and second vehicle axes of rotation.

5. Apparatus, as claimed in claim 4, wherein said means for generating comprises:

linear accelerometer means carried by said vehicle independent of said object for generating linear acceleration signals corresponding to the linear accelerations of said vehicle; and

processor means for calculating said rotational acceleration signals in response to said linear acceleration signals.

6. Apparatus, as claimed in claims 2 or 4, wherein said feedback signals comprise feedback rotational velocity signals corresponding to the rotational velocities of said object around said first and second object axes of rotation.

7. Apparatus, as claimed in claims 2 or 4, wherein said feedback signals comprises feedback rotational position signals corresponding to the rotational positions of said object around said first and second object axes of rotation.

8. Apparatus, as claimed in claim 1, wherein said object is capable of being rotated around first, second and third mutually orthogonal object axes and said vehicle defines first, second and third mutually orthogonal vehicle axes and wherein said movement means comprise:

first rotating means capable of rotating said object about said first object axis in response to a first one of said movement signals;

second rotating means capable of rotating said object about said second object axis in response to a second one of said movement signals;

third rotating means capable of rotating said object about said third object axis in response to a third one of said movement signals.

9. Apparatus, as claimed in claim 8, wherein said movement means comprises a mounting base attached to said vehicle and wherein said first rotating means comprises;

a first gimbal coupled to said base and capable of rotating about a first gimbal axis corresponding to said third vehicle axis and

first motor driving means for rotating said first gimbal in response to said first movement signal, wherein the second rotating means comprises;

a second gimbal coupled to said first gimbal and capable of rotating about a second gimbal axis orthogonal to said first gimbal axis and corresponding to said second vehicle axis, and

second motor driving means for rotating said second gimbal in response to said second movement signal, wherein the third rotating means comprises;

a third gimbal coupled to said second gimbal and capable of rotating about a third gimbal axis orthogonal to said second gimbal axis and corresponding to said first vehicle axis, and

third motor driving means for rotating said third gimbal in response to said third movement signal, and wherein said feedback means comprises;

a first transducer measuring the angle of rotation of said first gimbal around said first gimbal axis,

a second transducer measuring the angle of rotation of said second gimbal around said second gimbal axis and

a third transducer measuring the angle of rotation of said third gimbal around said third gimbal axis, and wherein said control system means is responsive to said vehicle rotation signals and to at least one of said first, second and third transducers for generating said first, second and third movement signals.

10. Apparatus, as claimed in claim 9, wherein said mounting base is passively isolated from said vehicle and said means for generating comprise linear accelerometers attached to said mounting base and arranged in a first group of linear accelerometers positioned at the intersection of three orthogonal base axes defined by said base corresponding to said axes of said vehicle, said first group of linear accelerometers measuring linear accelerations along said three orthogonal base axes, and second, third and fourth groups of linear accelerometers, each second, third and fourth group of linear accelerometers positioned along one of said three orthogonal base axes and measuring linear accelerations along three orthogonal axes.

11. Apparatus, as claimed in claim 9, wherein said mounting base is passively isolated from said vehicle and said means for generating comprise linear accelerometers attached to said mounting base and arranged in a first group of linear accelerometers positioned at the intersection of three orthogonal base axes defined by said base corresponding to said axes of said vehicle, said first group of linear accelerometers measuring linear accelerations along said three orthogonal base axes;

and second, third and fourth groups of linear accelerometers, each second, third and fourth group of linear accelerometers positioned along one of said orthogonal axes and measuring linear accelerations along axes parallel to the other two of said three orthogonal base axes.

12. Apparatus, as claimed in claim 9, wherein said mounting base is passively isolated from said vehicle and said means for generating comprise linear accelerometers attached to said mounting base and arranged in a first group of linear accelerometers positioned at the intersection of three orthogonal base axes defined by said base corresponding to said axes of said vehicle and measuring linear accelerations along first and second of said base axes corresponding to axes of said vehicle, a second group of linear accelerometers positioned along a third of said base axes corresponding to an axis of said vehicle and measuring linear accelerations along axes parallel to said first and second base axes, and a third linear accelerometer positioned along one of said base axes containing said first group of linear accelerometers and measuring linear accelerations along an axis corresponding to an axis of said vehicle and parallel to one of said first and second base axes.

13. Apparatus, as claimed in claim 9, wherein said third movement signal is responsive to a third, setpoint signal G₃, corresponding to the desired angular velocity of said object around said third gimbal axis and proportional to

14. Apparatus, as claimed in claim 9, wherein said apparatus is operated in a scanning mode and wherein said third movement signal is responsive to a third setpoint signal, G₃, corresponding to the desired angular velocity of said object around said third gimbal axis and proportional to

15. Apparatus, as claimed in claim 9, wherein said third movement signal is responsive to a third setpoint signal, G₃, corresponding to the desired angular acceleration of said object around said third gimbal axis and proportional to

16. Apparatus, as claimed in claim 9, wherein said apparatus is operated in a scanning mode and wherein said third movement signal is responsive to a third setpoint signal, G₃, corresponding to the desired angular acceleration of said object around said third gimbal axis and proportional to

17. A method for stabilizing an object around at least first and second object axes of rotation with respect to an inertial frame of reference, said object being carried by a vehicle subjected to rotational movement around at least first and second vehicle axes of rotation corresponding to said at least first and second object axes of rotation, said method comprising the steps of:

generating vehicle rotation signals corresponding to the rotational movement of said vehicle around at least said first and second vehicle axes of rotation with respect to said inertial frame of reference;

generating feedback signals corresponding to the movement of said object around at least said first and second object axes of rotation independent of said inertial frame of reference;

generating movement signals responsive to said one or more vehicle rotation signals and responsive to said feedback signals; and

rotatably moving said object around at least said first and second object axes responsive to said movement signals, whereby said object is stabilized around at least said first and second object axes with respect to said inertial frame of reference without the use of a gyroscope as said vehicle undergoes rotation relative to said inertial frame of reference.

18. A method, as claimed in claim 17, wherein said vehicle rotation signals comprise vehicle rotational velocity signals corresponding to the rotational velocities of said vehicle around at least said first and second vehicle axes of rotation.

19. A method, as claimed in claim 18, wherein said steps of generating comprises the steps of:

generating linear acceleration signals corresponding to the linear accelerations of said vehicle; and

calculating said rotational velocity signals in response to said linear acceleration signals.

20. A method, as claimed in claim 17, wherein said vehicle rotation signals comprises vehicle rotational acceleration signals corresponding to the rotational accelerations of said vehicle around at least said first and second vehicle axes of rotation.

21. A method, as claimed in claim 20, wherein the step of generating comprises the steps of:

generating linear acceleration signals corresponding to the linear accelerations of said vehicle; and

calculating said rotational acceleration signals in response to said linear acceleration signals.

22. A method, as claimed in claims 18 or 20, wherein the feedback signals comprise feedback rotation velocity signals corresponding to the rotational velocities of said object around at least said first and second object axes of rotation.

23. A method, as claimed in claims 18 or 20, wherein the feedback signals comprises feedback rotational position signals corresponding to the rotational positions of said object around at least said first and second object axes of rotation.

24. A method, as claimed in claim 17, wherein said vehicle axes of rotation are orthogonal vehicle axes of rotation, wherein said object is moved relative to said vehicle by rotation around first, second and third orthogonal object axes of rotation and said movement signals comprise first, second and third movement signals for rotation around said first, second and third orthogonal object axes of rotation, respectively, and wherein said third movement signal is responsive to a third setpoint signal, S₃ proportional to

25. A method, as claimed in claim 17, wherein said vehicle axes of rotation comprise orthogonal vehicle axes of rotation, wherein said object is moved in a scanning mode relative to said vehicle by rotation around first, second and third orthogonal object axes of rotation and said movement signals comprise first, second and third movement signals for rotation around said first, second and third orthogonal object axes of rotation, respectively, and wherein said third movement signal is responsive to a third setpoint signal, S₃, proportional to

26. A method, as claimed in claim 17, wherein said vehicle axes of rotation are orthogonal vehicle axes of rotation, wherein said object is moved relative to said vehicle by rotation around first, second and third orthogonal object axes of rotation and said movement signals comprise first, second, and third movement signals for rotation around said first, second, and third orthogonal object axes of rotation, respectively, and wherein said third movement signal is responsive to a third setpoint signal, S₃ proportional to

27. A method, as claimed in claim 17, wherein said vehicle axes of rotation comprise orthogonal vehicle axes of rotation, wherein said object is moved in a scanning mode relative to said vehicle by rotation around first, second and third orthogonal object axes of rotation and said movement signals comprise first, second, and third movement signals for rotation around said first, second, and third orthogonal object axes of rotation, respectively, and wherein said third movement signal is responsive to a third setpoint signal, S₃ proportional to

28. Apparatus for stabilizing an object capable of being rotated in three degrees of freedom with respect to an inertial frame of reference, said object being carried in a vehicle subject to rotational movement around first, second and third vehicle axes of rotation with respect to said inertial frame of reference, said object defining three object axes corresponding to said first, second and third vehicle axes of rotation, said apparatus comprising in combination:

linear accelerometer means carried by said object for measuring the net linear accelerations of said object and said vehicle in said three degrees of freedom;

processor means for calculating the net angular accelerations of said object and said vehicle in said three degrees of freedom in response to said linear accelerometer means;

control system means responsive to said calculating of said net angular accelerations by said processor means for generating movement signals; and

movement means responsive to said movement signals for rotatably moving said object in said three degrees of freedom, whereby said object is stabilized in said three degrees of freedom with respect to said inertial frame of reference without the use of a gyroscope as said vehicle undergoes rotation relative to said inertial frame of reference.

29. Apparatus, as claimed in claim 28, and further comprising feedback means for generating feedback signals corresponding to the movement of said object with respect to said object coordinate axes in said three degrees of freedom wherein said control system means is responsive to said processor means and said feedback signals for generating said movement signals.

30. Apparatus, as claimed in claim 29, wherein said feedback signals comprise feedback rotational velocity signals corresponding to the rotational velocities of said object with respect to said object coordinate axes in said three degrees of freedom.

31. Apparatus, as claimed in claim 29, wherein said feedback signals comprise feedback rotational position signals corresponding to the rotational position of said object with respect to said object coordinate axes in said three degrees of freedom.

32. Apparatus, as claimed in claim 28, wherein said object coordinate axes comprise roll, pitch and yaw axes, wherein said object is rotatable around said roll, pitch and yaw axes, wherein the means for calculating comprises means for calculating the net angular accelerations of said object and said vehicle around said roll, pitch and yaw axes, and wherein the control system means comprises means for generating movement signals such that the net angular accelerations of said object and said vehicle around said roll, pitch and yaw axes are urged toward respective nominal values.

33. Apparatus, as claimed in claim 32, wherein said movement means comprises:

means for maintaining, increasing or decreasing the acceleration of said object around said roll axis depending on whether the means for calculating indicates that the net acceleration of said object and said vehicle around said roll axis is equal to, less than or greater than, respectively, said nominal value;

means for maintaining, increasing or decreasing the acceleration of said object around said pitch axis depending on whether the means for calculating indicates that the net acceleration of said object and said vehicle around said pitch axis is equal to, less than or greater than, respectively, said nominal value; and

means for maintaining, increasing or decreasing the acceleration of said object around said yaw axis depending on whether the means for calculating indicates that the net acceleration of said object and said vehicle around said yaw axis is equal to, less than or greater than, respectively, said nominal value.

34. Apparatus, as claimed in claim 28, wherein said object axes are orthogonal object axes, wherein said linear accelerometer means comprises linear accelerometers attached to said object and arranged in a first group of linear accelerometers positioned at the intersection of said three orthogonal object axes, said first group of linear acclerometers measuring linear accelerations along axes parallel to said three orthogonal object axes, and second, third, and fourth groups of linear accelerometers, each second, third and fourth groups of linear accelerometers positioned along one of said three orthogonal object axes and measuring linear accelerations along said three orthogonal object axes.

35. Apparatus, as claimed in claim 28, wherein said object axes are orthogonal object axes, wherein said linear accelerometer means comprises linear accelerometers attached to said object and arranged in a first group of linear accelerometers positioned at the intersection of said three orthogonal object axes, said first group of linear accelerometers measuring linear accelerations along said three orthogonal object axes, and second, third, and fourth groups of linear accelerometers, each second, third and fourth groups of linear accelerometers positioned along one of said three orthogonal object axes and measuring linear accelerations along axes parallel to the other two of said three orthogonal object axes.

36. Apparatus, as claimed in claim 28, wherein said object axes are orthogonal object axes, wherein said linear accelerometer means comprises linear accelerometers attached to said object and arranged in a first group of linear accelerometers positioned at the intersection of said three orthogonal object axes, said first group of linear accelerometers measuring linear accelerations along first and second object axes of said orthogonal object axes;

a second group of linear accelerometers positioned along a third object axis of said object axes and measuring linear acceleration along axes parallel to said first and second object axes, and a third linear accelerometer positioned along an object axis containing said first group of linear accelerometers and measuring linear accelerations parallel to one of said first and second axes of said orthogonal object axes.

37. A method of stabilizing an object capable of being rotated in three degrees of freedom with respect to an inertial frame of reference, said object being carried in a vehicle subject to rotational movement around first, second and third vehicle axes of rotation with respect to said inertial frame of reference, said object defining three object axes corresponding to said first, second and third vehicle axes of rotation, said method comprising the steps of:

measuring the net linear accelerations of said object and said vehicle in said three degrees of freedom;

calculating the net angular accelerations of said object and said vehicle in said three degrees of freedom in response to said measurement of net linear accelerations;

generating movement signals responsive to said calculating of said net angular accelerations; and

rotatably moving said object in said three degrees of freedom responsive to said movement signals, whereby said object is stabilized in said three degrees of freedom with respect to said inertial frame of reference without the use of a gyroscope as said vehicle undergoes rotation relative to said inertial frame of reference.

38. A method, as claimed in claim 37, and further comprising the steps of:

generating feedback signals corresponding to the movement of said object with respect to said object axes in said three degrees of freedom; and

generating said movement signals responsive to said angular acceleration and said feedback signals.

39. A method, as claimed in claim 38, wherein said feedback signals comprise feedback rotational velocity signals corresponding to the rotational velocities of said object with respect to said object axes in said three degrees of freedom.

40. A method, as claimed in claim 38, wherein said feedback signals comprise feedback rotational position signals corresponding to the rotational positions of said object with respect to said object axes in said three degrees of freedom.

41. A method, as claimed in claim 37, wherein said object axes comprise roll, pitch and yaw axes, wherein said object is rotatable around said roll, pitch and yaw axes, wherein the step of calculating comprises the step of calculating the net angular accelerations of said object and said vehicle around said roll, pitch and yaw axes, and wherein the step of generating comprises the step of generating movement signals such that the net angular accelerations of said object and said vehicle around said roll, pitch and yaw axes are urged toward respective nominal values.

42. A method, as claimed in claim 41, wherein said step of rotatably moving comprises the steps of:

maintaining, increasing or decreasing the acceleration of said object around said roll axis depending on whether the step of calculating indicates that the net acceleration of said object and said vehicle around said roll axis is equal to, less than or greater than, respectively, said nominal value;

maintaining, increasing or decreasing the acceleration of said object around said pitch axis depending on whether the step of calculating indicates that the net acceleration of said object and said vehicle around said pitch axis is equal to, less than or greater than, respectively, said nominal value; and

maintaining, increasing or decreasing the acceleration of said object around said yaw axis depending on whether the step of calculating indicates that the net acceleration of said object and said vehicle around said yaw axis is equal to, less than or greater than, respectively, said nominal value.