Method and GNC system for determination of roll angle

Patent metadata

Field	Value
Publication number	US-9354028-B2
Application number	US-201214345791-A
Country	US
Kind code	B2
Filing date	Sep 13, 2012
Priority date	Sep 20, 2011
Publication date	May 31, 2016
Grant date	May 31, 2016

Abstract

The invention relates to a method for determining the roll angle of a guidable and substantially or partially roll-stable projectile comprising control system, radio-based positioning receiver and sensor for measuring roll angular velocity, in which the following steps are included: actuation of the actuators of the projectile by the control system, included in the projectile, for maneuvering of the projectile; estimation of a first signal, the projectile control force, on the basis of the control system included in the projectile; measurement of a second signal, the velocity of the projectile relative to the ground-fixed coordinate system, with the radio-based positioning receiver mounted in the projectile; measurement of a third signal, the rotational velocity, with the sensor for roll angular velocity mounted in the projectile; calculation of a roll angle on the basis of the first, second and third signals, estimated projectile control force, measured projectile velocity, and measured rotational velocity, by summation of the absolute angle change with weighting of an angle evaluation. The invention additionally relates to a GNC system for a guidable projectile comprising control system, radio-based positioning system, and a sensor for measuring roll angular velocity.

First claim

What is claimed is:

1. Method for determining the roll angle of a guidable and substantially or partially roll-stable projectile comprising control system, radio-based positioning receiver and sensor for measuring roll angular velocity, which comprises the following steps:
(a) actuation of the actuators of the projectile by the control system, included in the projectile, for maneuvering of the projectile;
(b) estimation of a first signal, the projectile control force, on the basis of the control system included in the projectile;
(c) measurement of a second signal, the velocity of the projectile relative to the ground-fixed coordinate system, with the radio-based positioning receiver mounted in the projectile;
(d) measurement of a third signal, the rotational velocity, with the sensor for roll angular velocity mounted in the projectile;
(e) calculation of a roll angle on the basis of the first, second and third signals, estimated projectile control force, measured projectile velocity and measured rotational velocity, by summation of the absolute angle change with weighting of an angle evaluation.

2. Method for roll angle determination according to claim 1 , wherein the absolute angle change is set to correspond to the resultant angle of the change in pitch angle of the projectile velocity vector and the change in yaw angle of the projectile velocity vector.

3. Method for roll angle determination according to claim 1 , wherein the angle evaluation is perceived as a mean value of the angle of incidence evaluation.

4. Method for roll angle determination according to claim 3 , wherein the mean value of the angle of incidence evaluation is assumed to correspond to the mean value of the resultant angle of the projectile control force which controls the yaw component, β, of the angle of incidence and the projectile control force which controls the pitch component, α, of the angle of incidence.

5. Method for roll angle determination according to claim 1 , wherein the angle evaluation is perceived as a mean value of the angle of the control force angle evaluation.

6. Method for roll angle determination according to claim 5 , wherein the mean value of the control force angle evaluation is assumed to correspond to the mean value of the resultant angle of the projectile control force which controls the yaw component of the velocity vector and the projectile control force which controls the pitch component of the velocity vector.

7. Method for roll angle determination according to claim 1 , wherein calculation is made with filtering.

8. Method for roll angle determination according to claim 1 , wherein the sensor for measuring roll angular velocity is a gyroscope.

9. Method for roll angle determination according to claim 1 , wherein the radio-based positioning receiver is a GPS receiver.

10. Method for roll angle determination according to claim 1 , wherein pitch angle, θ, is calculated by summation of the resultant of the projectile velocity components measured by the radio-based positioning system and evaluation of the projectile control force which controls the pitch component, α, of the angle of incidence.

11. Method for roll angle determination according to claim 1 , wherein pitch angle, θ, is calculated by summation of the resultant of the projectile velocity components measured by the radio-based positioning system and evaluation of the projectile control force which controls the pitch component of the velocity vector.

12. Method for roll angle determination according to claim 1 , wherein yaw angle, ψ, is calculated by subtraction of the evaluation of the projectile control force which controls the yaw component, β, of the angle of incidence from the resultant of the projectile velocity components measured by the radio-based positioning system.

13. Method for roll angle determination according to claim 1 , wherein yaw angle, ψ, is calculated by subtraction of the evaluation of the projectile control force which controls the yaw component of the velocity vector from the resultant of the projectile velocity components measured by the radio-based positioning system.

14. GNC system for a guidable projectile comprising control system, radio-based positioning system and sensor for measuring roll angular velocity for determination of roll angle, wherein;
(a) the incorporated control system for maneuvering of the projectile is arranged to actuate the actuators of the projectile;
(b) the control system included in the projectile is arranged to estimate a first signal, projectile control force;
(c) the radio-based positioning receiver mounted in the projectile measures a second signal, the velocity of the projectile relative to the ground-fixed coordinate system;
(d) the sensor for roll angular velocity mounted in the projectile measures a third signal, rotational velocity;
(e) the first, second and third signals, estimated projectile control force, measured projectile velocity and measured rotational velocity, together calculate a roll angle, in the GNC system, by summation of the absolute angle change with weighting of an angle evaluation.

15. GNC system for guidable projectile according to claim 14 , wherein the absolute angle change is set to correspond to the resultant angle of the change in pitch angle of the projectile velocity vector and the change in yaw angle of the projectile velocity vector.

16. GNC system for guidable projectile according to claim 14 , wherein the angle evaluation is perceived as a mean value of the angle of incidence evaluation.

17. GNC system for guidable projectile according to claim 16 , wherein the mean value of the angle of incidence evaluation is assumed to correspond to the mean value of the resultant angle of the projectile control force which controls the yaw component, β, of the angle of incidence and the projectile control force which controls the pitch component, α, of the angle of incidence.

18. GNC system for guidable projectile according to claim 14 , wherein the angle evaluation is perceived as a mean value of the angle of the control force angle evaluation.

19. GNC system for guidable projectile according to claim 18 , wherein the mean value of the control force angle evaluation is assumed to correspond to the mean value of the resultant angle of the projectile control force which controls the yaw component of the velocity vector and the projectile control force which controls the pitch component of the velocity vector.

20. GNC system for guidable projectile according to claim 14 calculation is made with filtering.

21. GNC system for guidable projectile according to claim 14 , wherein the sensor for measuring roll angular velocity is a gyroscope.

22. GNC system for guidable projectile according to claim 14 , wherein the radio-based positioning receiver is a GPS receiver.

23. GNC system for guidable projectile according to claim 14 , wherein pitch angle, θ, is calculated by summation of the resultant of the projectile velocity components measured by the radio-based positioning system and evaluation of the projectile control force which controls the pitch component, α, of the angle of incidence.

24. GNC system for guidable projectile according to claim 14 , wherein pitch angle, θ, is calculated by summation of the resultant of the projectile velocity components measured by the radio-based positioning system and evaluation of the projectile control force which controls the pitch component of the velocity vector

Assignees

• Brohede Daniel
• Bae Systems Bofors Ab

Inventors

• Brohede Daniel

Classifications

• G01C21/165

  combined with non-inertial navigation instruments · CPC title

• G05D1/108

  animated with a rolling movement · CPC title

• F42B15/01 Primary

  Arrangements thereon for guidance or control ({steering arrangements F42B10/60}; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]) · CPC title

• F41G7/305

  for spin-stabilized missiles · CPC title

• F41G9/00 Primary

  Systems for controlling missiles or projectiles, not provided for elsewhere · CPC title