Stabilized weapon platform with active sense and adaptive motion control
A stabilized platform is provided with active sense and adaptive control is provided that allows an operator, during operation, to switch between an electrically assisted operational mode to a manual operational mode. Related systems, apparatus, methods, and articles are also described.
1. An apparatus comprising:
a stabilization assembly comprising one or more gimbals configured to be moved in one or more directions relative to a host platform;
a payload cradle mounted to the assembly and configured to secure a payload mounted thereon;
two or more electrical motion control actuators;
one or more motion sensors sensing motion of the assembly in one or more inertial degrees of freedom;
a control processor electrically interfaced with the two or more electrical motion control actuators and the one or more motion sensors; and
an interface selector control that enables selective switching between first and second operating modes during operation,
wherein:
in the first operating mode, the control processor automatically commands the two or more electrical motion control actuators based on motion data provided by the one or more motion sensors to stabilize an aim point of the payload by correcting for changes in payload aim caused by motion,
in the second operating mode, the control processor automatically commands at least one of the two or more motion control actuators to disengage such that the payload and its assembly may be freely slewed by an operator.
2. The apparatus of claim 1 , wherein the interface selector control is mounted to the payload cradle or the payload.
3. The apparatus of claim 1 , wherein the one or more gimbals are provided for selectively positioning the payload.
4. The apparatus of claim 1 , wherein there are one or more payload controls provided for operation of the payload.
5. The apparatus of claim 4 , wherein the one or more payload controls are mounted to or form part of the payload.
6. The apparatus of claim 4 , wherein the one or more payload controls are mounted to or form part of the cradle or assemble.
7. The apparatus of claim 4 , wherein the control processor determines, based on data received from the one or more motion sensors, whether or not an operator is manning the payload.
8. The apparatus of claim 7 , wherein the control processor determines, based on the data received from the one or more motion sensors, whether or not the operator has one hand or two hands on the payload controls.
9. The apparatus of claim 1 , wherein the one or more gimbal controls that are configured adjust the aim point of the payload while in the first operating mode.
10. The apparatus of claim 1 , wherein the payload is a crew-served weapon.
11. The apparatus of claim 1 , wherein the payload is a camera or a light source.
12. The apparatus of claim 1 , wherein the one or more motion sensors comprise at least one sensor selected from a group consisting of: inertial navigation systems (INS), global positioning systems (GPS), global navigation systems (GNSS), magnetometers, inclinometers, range finders, and radar sensors.
13. The apparatus of claim 1 , further comprising an environmental sensor measuring at least one attribute selected from a group consisting of: altitude, temperature, humidity, air pressure, wind conditions in direction and/or magnitude.
14. The apparatus of claim 1 , wherein the host platform is secured to a moveable vehicle.
15. The apparatus of claim 1 , wherein the host platform is subject to motion comprising (i) rotational motion, (ii) linear motion, or (iii) a combination of rotational and linear motion.
16. The apparatus of claim 1 , wherein a first actuator comprises an elevation actuator, and a second actuator comprises an azimuth actuator.
17. The apparatus of claim 1 , wherein a first motion sensor comprises an elevation sensor and the second motion sensor comprises an azimuth sensor.
18. The apparatus of claim 1 , wherein the payload cradle has two degrees of freedom relative to the host platform comprising azimuth and elevation.
19. The apparatus of claim 1 , wherein motion relative to Earth is measured as well as the motion of the payload relative to the host platform.
20. The apparatus of claim 1 , wherein movement of the payload may be operated remotely by an operator.
21. The apparatus of claim 1 , wherein the one or more motion sensors comprise a plurality of axis motion sensors comprising a gyroscope, an accelerometer, or a combination thereof.
22. The apparatus of claim 21 , wherein the one or more motion sensors detect motion in at least one of six degrees of freedom comprising pitch, roll, yaw, x, y, or z.
23. The apparatus of claim 1 , further comprising one or more target characterization sensors to generate data characterizing one or more of the motion, range, and speed of a target.
24. A method comprising:
initiating operation of stabilized platform in a first operating mode, the stabilization platform comprising:
a stabilization assembly comprising one or more gimbals configured to be moved in one or more directions relative to a host platform;
a payload cradle mounted to the assembly and configured to secure a payload mounted thereon;
two or more electrical motion control actuators;
one or more motion sensors sensing motion of the assembly in one or more inertial degrees of freedom;
a control processor electrically interfaced with the two or more electrical motion control actuators and the one or more motion sensors; and
an interface selector control that enables selective switching between first and second operating modes during operation,
receiving, by the interface selector, a signal or input switching to the second operating mode; and
initiating operation of the stabilized platform in the second operating mode;
wherein:
in the first operating mode, the control processor automatically commands the two or more electrical motion control actuators based on motion data provided by the one or more motion sensors to stabilize an aim point of the payload by correcting for changes in payload aim caused by motion,
in the second operating mode, the control processor automatically commands at least one of the two or more motion control actuators to disengage such that the payload and its assembly may be freely slewed by an operator.