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Inertial stabilization controller

An inertial stabilization and controller technology, applied in the field of aero-optical remote sensing, can solve the problems of uncertainty in the selection of actuators, sensors and quantities, incompatibility with digital or analog sensors, poor versatility and inheritance, etc. The effect of wide range, high driving power and strong compatibility

Active Publication Date: 2015-04-08
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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AI Technical Summary

Problems solved by technology

The current motor controller is relatively mature, but the motor driver in the inertial space in the field of aviation remote sensing is not yet mature, especially for multi-axis, multi-sensor, and multi-functional drivers. There are still the following problems: (1) According to the different requirements of the indicators , the selected actuators, sensors and quantities are uncertain, and different drive modules and acquisition modules need to be configured for different projects; (2) The versatility and inheritance are poor, and the sensors that cannot be compatible are digital or analog, which is not conducive to Sensor Replacement

Method used

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Embodiment Construction

[0032] The specific embodiment of the present invention is described in further detail below in conjunction with accompanying drawing:

[0033] Both the inertial stability controller and the inertial platform are mounted on the carrier, and the inertial stability controller is used to control the stability of the inertial platform on the carrier. figure 1 It is a system block diagram of the inertial stability controller of the present invention, including a main control module, an azimuth motor drive module, a pitch motor drive module, a roll motor drive module, a rate gyro acquisition module, an angular position acquisition module, E 2 PROM data storage module, serial port expansion module, management control module, inertial navigation module and secondary power supply module.

[0034] The inertial navigation module is fixedly connected to the carrier through four installation ports, and after installation, the X-axis of the inertial navigation module points to the carrier c...

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Abstract

The invention discloses an inertial stabilization controller. The inertial stabilization controller comprises a main control module, an orientation motor driving module, a pitching motor driving module, a roll motor driving module, a rate gyro acquisition module, an angular position acquisition module, a data storage module, a serial port expansion module, a management control module, an inertial navigation module and a secondary power source module. The inertial stabilization controller integrates functions of driving, acquisition, storage, communication and synchronization into one body and greatly ameliorates a problem of single function of an inertial stabilization controller in the prior art. The inertial stabilization controller can eliminate influence of high carrier aircraft and low frequency disturbance on pendular or tracking imaging systems, is applicable to a single-axis, two-axis or three-axis inertial stabilization platform, has a wide application scope and is successfully applied to multiple models of aviation optical remote sensors.

Description

technical field [0001] The invention relates to a multi-axis multi-functional high-precision inertial stability controller, which belongs to the technical field of aerial optical remote sensing. Background technique [0002] In the field of aerial remote sensing, the imaging system is often subject to external disturbances, such as wind speed, vibration of the aircraft, etc., which will greatly reduce the imaging quality. In order to ensure imaging stability in inertial space, a general inertial stability controller is proposed. In the past, most controllers used a single-axis or dual-axis stable structure, that is, to control the movement of the visual axis along two rotational degrees of freedom that are orthogonal to the visual axis and perpendicular to each other, and keep the visual axis stable. However, this dual-axis stabilized platform Ignoring the disturbance of the third direction axis, it can only be applied to the case where the external environment has little i...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D3/12
Inventor 宋立国王哲陈凌军李兵
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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