Methods and apparatus for swash plate guidance and control

• US 6,360,987 B1
• Filed: 05/23/2000
• Issued: 03/26/2002
• Est. Priority Date: 05/23/2000
• Status: Expired due to Fees

• Current Assignee: BAE Systems Integrated Defense Solutions, Inc
• Original Assignee: BAE Systems Integrated Defense Solutions (BAE Systems Plc)
• Inventors: Sallaee, Bradley T., Vinson, Ken
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/578,800
• Time in Patent Office: 672 Days
• Field of Search: 244/90.R, 244/3.23, 244/3.24, 244/3.22, 244/3.21, 416/98, 416/99, 416/108
• US Class Current: 244/3.21
• CPC Class Codes: F42B 10/26 using spin F42B10/04, F42B10/12, F42B10/14, F42B10/24, F42B14/02 take precedence
• CPC Class Codes: F42B 10/54 Spin braking means
• CPC Class Codes: F42B 15/01 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]

Abstract

Apparatuses and methods for controlling an object spinning at a first rate in a first direction. The apparatus includes a swash plate, a rotor, a spin actuator, a roll actuator, and a pitch actuator. The rotor is coupled to the swash plate. The spin actuator is coupled to the rotor and is configured to spin the rotor in a second direction opposite the first direction at a second rate. The roll actuator is coupled to the rotor and is configured to displace the swash plate along a longitudinal axis. The pitch actuator is coupled to the rotor and is configured to tilt the swash plate in a tilt direction about the longitudinal axis, the tilt direction being adjustable by adjusting the second rate relative to the first rate. The roll actuator may be coupled to the pitch actuator so that the pitch actuator keeps a substantially identical orientation with the swash plate as the swash plate is displaced along the longitudinal axis by the roll actuator.

Claims

1. An apparatus for controlling an object spinning at a first rate in a first direction, comprising:

a swash plate;

a rotor coupled to the swash plate;

a spin actuator coupled to the rotor and configured to spin the rotor in a second direction opposite the first direction;

a roll actuator coupled to the rotor and configured to displace the swash plate along a longitudinal axis; and

a pitch actuator coupled to the rotor and configured to tilt the swash plate in a tilt direction about the longitudinal axis.

2. The apparatus of claim 1, wherein the spin actuator is configured to spin the rotor at a second rate substantially equal the first rate.

3. The apparatus of claim 1, further comprising one or more control rods coupled to the swash plate, the control rods being configured to couple to one or more guidance members of the object.

4. The apparatus of claim 1, the spin actuator being configured to spin the rotor in the second direction at a third rate not equal to the second rate to adjust the tilt direction.

5. The apparatus of claim 1, wherein the spin actuator comprises:

a spin motor;

a spin pinion coupled to the motor;

a spin gear coupled to the pinion; and

a spline drive coupled to the gear and to the rotor.

6. The apparatus of claim 1, wherein the roll actuator comprises:

a roll motor;

a roll pinion coupled to the motor;

a roll gear coupled to the pinion; and

a roll drive screw coupled to the gear and to the rotor.

7. The apparatus of claim 1, wherein the pitch actuator comprises:

a pitch motor;

a pitch pinion;

a pitch gear coupled to the pinion; and

a pitch bearing coupled to the gear and to the rotor.

8. The apparatus of claim 1, wherein the pitch actuator is coupled to a roll drive screw.

9. The apparatus of claim 1, wherein the object is a missile.

10. An apparatus for controlling an object spinning at a first rate in a first direction, comprising:

a swash plate;

a rotor coupled to the swash plate;

a spin actuator coupled to the rotor and configured to spin the rotor in a second direction opposite the first direction at a second rate;

a roll actuator coupled to the rotor and configured to displace the swash plate along a longitudinal axis; and

a pitch actuator coupled to the rotor and configured to tilt the swash plate in a tilt direction about the longitudinal axis, the tilt direction being adjustable by adjusting the second rate relative to the first rate;

wherein the roll actuator is coupled to the pitch actuator so that the pitch actuator keeps a substantially identical orientation with the swash plate as the swash plate is displaced along the longitudinal axis by the roll actuator.

11. The apparatus of claim 10, wherein the second rate is substantially equal the first rate.

12. The apparatus of claim 10, further comprising one or more control rods coupled to the swash plate, the control rods being configured to couple to one or more guidance members of the object.

13. The apparatus of claim 10, wherein the spin actuator comprises:

a spin motor;

a spin pinion coupled to the motor;

a spin gear coupled to the pinion; and

a spline drive coupled to the gear and to the rotor.

14. The apparatus of claim 10, wherein the roll actuator comprises:

a roll motor;

a roll pinion coupled to the motor;

a roll gear coupled to the pinion; and

a roll drive screw coupled to the gear and to the rotor.

15. The apparatus of claim 10, wherein the pitch actuator comprises:

a pitch motor;

a pitch pinion;

a pitch gear coupled to the pinion; and

a pitch bearing coupled to the gear and to the rotor.

16. The apparatus of claim 10, wherein the roll actuator and the pitch actuator are coupled to a roll drive screw.

17. The apparatus of claim 10, wherein the object is a missile.

18. A method for controlling an object spinning at a first rate in a first direction, comprising:

coupling one or more guidance members of the object to a swash plate;

spinning a rotor coupled to the swash plate in a second direction opposite the first direction at a second rate substantially equal the first rate; and

tilting the swash plate about a longitudinal axis with a pitch actuator coupled to the rotor to affect a change in pitch of the object.

19. The method of claim 18, wherein the coupling comprises coupling one or more fins to one or more control rods coupled to the swash plate.

20. The method of claim 18, further comprising displacing the swash plate along a longitudinal axis with a roll actuator to affect a change in the first rate.

21. The method of claim 20, wherein the displacing the swash plate does not substantially affect the orientation of the pitch actuator with the swash plate.

22. The method of claim 18, wherein the object is a missile.

23. A method for controlling an object spinning at a first rate in a first direction, comprising:

coupling one or more guidance members of the object to a swash plate;

spinning a rotor coupled to the swash plate in a second direction opposite the first direction at a second rate;

tilting the swash plate in a first tilt direction about a longitudinal axis with a pitch actuator coupled to the rotor to affect a first change in pitch of the object;

spinning the rotor in the second direction at a third rate to adjust the first tilt direction to a second tilt direction about the longitudinal axis; and

tilting the swash plate in the second tilt direction with the pitch actuator to affect a second change in pitch of the object.

24. The method of claim 23, wherein the coupling comprises coupling one or more fins to one or more control rods coupled to the swash plate.

25. The method of claim 23, further comprising displacing the swash plate along a longitudinal axis with a roll actuator to affect a change in the first rate.

26. The method of claim 25, wherein the displacing the swash plate does not substantially affect the orientation of the pitch actuator with the swash plate.

27. The method of claim 23, wherein the object is a missile.