Device for Stabilizing of a Remotely Controlled Sensor, Like a Camera

The present invention relates to a device for stabilizing of a remotely controlled sensor, of the art disclosed in the preamble of enclosed 1:st patent claim.

In civil and military contexts surveillance towards an object for achieving information of some art are common. The surveillance is usually performed by some type of sensor, e g a video camera, an infrared camera or the like. The sensor is usually mounted at a vehicle, i e a boat, an automobile, an aircraft, a helicopter etc. in order to facilitate the surveillance the sensor is usually remotely controlled from an operator's site in the vehicle. As the vehicle normally moves, and this also is the case for the object, thus the sensor has to be remotely controlled. The degrees of freedom are primarily two, that is to say in yaw (azimuth) and pitch (elevation). In this design the aiming line of the sensor can be directed towards the object. When the vehicle moves, the operator has no time to continuously compensate by remote control for occurring angle deviations between the aiming line of the sensor and the object The result is, that the object gets outside of the aiming line of the sensor, or that the image created by the sensor of the object will not be sharp. Until now this problem has been solved by providing the sensor with a two-axes electrical rategyro, which momentarily measures the angle error, that the sensor is subject to, and by controlling the space position of the sensor with an electronic system, so that this space position remains stable. This constructive solution is very expensive as it has to comprise mechanics of a high precision, servo systems of a high class and rate gyros with good function.

The object of the present invention is to achieve a device of the art disclosed in the preamble of the enclosed 1:st patent claim, provided with components of reasonable costs, yet with equally good function as devices designed according to the constructional solution just mentioned.

According to the invention, such a device is characterized primarily in that a mechanical coupling, comprising a resilient coupling means, connects the first gimbal to the third gimbal,

The invention will be described more in detail, reference being made to the attached perspective figures, of which:

FIG. 1 shows an embodiment of a device according to the invention,

FIG. 2 shows a stand, comprised in the device in FIG. 1,

FIG. 3 shows a three-axes right-angular coordinate system with the directions x, y and z,

FIG. 4 shows a special embodiment of the stand in FIG. 2.

In FIG. 1 a sensor, in this case a video camera, is denoted by 1. It is provided with a two-axes, i e in yaw and pitch stabilizing self-acting rategyro 2, and the sensor is arranged as an inner first gimbal 1, rotatable around a first yaw axis 3. This is journalled in a second gimbal 4, which is rotatable around a first pitch axis 5. This is journalled in an outer, third gimbal 6, rotatable around a second pitch axis 7, journalled in a fourth gimbal 8. This is rotatable around a second yaw axis 9. A first set motor 10 is fastened to the fourth gimbal and is provided to set the angle position of the second pitch axis 7. A second set motor 11 is fastened to a stand 12, which in turn is fastened to a vehicle like a helicopter. This second set motor 11 is provided to set the angle position of the second yaw axis 9. A first electric rategyro 13 is fastened to the stand 12 to sense the yaw angle rate and a second electric rategyro 14 is fastened to the fourth gimbal 8 to sense the pitch angle rate. A electronic unit 15 receives signals from said rategyros and controls the first and the second set motor 10 resp 11 so that these act stabilizing on the third gimbal 6 and the fourth gimbal 8. The set motors 10 and 11 can also be acted upon to set the sensor 1 in pitch and yaw by signals from a set means 16, via the electronic unit 15.

A mechanical coupling, comprising an arm 17 directed perpendicularly to the plane of the first yaw axis and the first pitch axis 5 from the intersecting point of these is provided with a resilient coupling means 16 at the rotational area (surface edge) of the third gimbal 6. The coupling means consists, in this embodiment, of a plate of an elastomer like polyurethane foam in the center embracing the end of the arm 17. Depending on the design and the application the stiffness of the foam respecting the spring constant of the springs, if such are utilized, have to be adapted to the demand. Generally it can be said, that the stabilizing, self-acting rategyro has for an object to compensate vibrations down to about 12 Hz, whilst the control device, comprising rategyros, set motors and electronic unit just described has for an object to compensate for more low-frequent vibrations. The direction of the arm 17 does not have to be the one described, but the more the direction deviates from the said one, the worse the function will be.

In FIG. 2 the stand 12 is shown more in detail. The stand comprises an upper frame 18, intended to be fastened to a vehicle, and a lower frame 19. Both frames are rectangular. At the corners they are connected by four spring elements 31, 32, 33 and 34. The lower frame is thus resiliently movable in a three-axes right-angular coordinate system with the directions x, y and z, as is shown in FIG. 3. The lower frame is also to some degree turnable in relationship to the upper frame. By the aid of a special design the parallelity between the frames is also retained in all directions of movement of the lower frame in relationship to the upper frame.

In the upper frame 18 there are namely, at two opposed sides, turnably journalled a first and a second torsion axis 20, 21, extending along the entire length of the the first frame 18. At the outer ends of the torsion axes there are provided, at right angle to the torsion axes, in the direction inward to the frame, four torsion arms. The first 22 and the second 23 are fastened at one end of the first resp the second torsion axis 20, 21, whilst the third 24 and the fourth 25 are fastened to the other end of the first resp the second torsion axis 20, 21. First and second links 26 and 27 are journalled at two ends, with one end at the first resp the second torsion arm 22, 23 and with the other end journalled at the lower frame 19, whilst the third arm torsion arm 24, at a distance from its outer end is connected to the lower frame 19 via a third link 28, journalled at two ends. The fourth torsion arm 25 is, at a distance from its outer end connected to the lower frame 19, via a fourth link 29, journalled at two ends, whilst the the third and fourth torsion arms 24 and 25 in their outer ends are swingably connected to a fifth link 30, journalled at two ends. The bearings of the links are such, that some movement at right angle to their plane of rotation is allowed.

The spring elements 31-34 admit, per se, a certain resilient stability laterally, but in order to warrant this, a device according to the invention as in FIG. 4 may be provided. A column 35 is stiffly fastened to the lower frame at the middle of its horizontal plane. It is directed vertically upwards towards the upper frame 18, and fifth to eighth spring elements 36, 37, 38 and 39 forming a resilient cross, connect the upper portion of the column with the sides of the upper frame. With this arrangement the lower frame is retained resiliently in its lateral position in relationship to the upper frame, whilst a certain mutual rotational movability between the frames is retained.