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Dual-super-satellite platform load cabin compound control method

A satellite platform and composite control technology, which is applied in the direction of space navigation vehicle guidance devices, space navigation equipment, space navigation aircraft, etc. The effect of state accuracy

Inactive Publication Date: 2018-05-18
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] In view of the deficiencies in the prior art, the purpose of the present invention is to provide a composite control method for the load cabin of a dual-super satellite platform that can effectively solve the problem that the load pointing accuracy and stability are difficult to be greatly improved

Method used

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  • Dual-super-satellite platform load cabin compound control method
  • Dual-super-satellite platform load cabin compound control method

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Embodiment Construction

[0036] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0037] Such as figure 1 As shown, the "Double Ultra" satellite is composed of a payload compartment 1 and a platform compartment 2. The payload compartment is installed with but not limited to payload 13, fiber optic gyroscope 11, star sensor 12, maglev mechanism stator and other quiet components, and the platform compartment is installed with but not limited to Solar panels 24 and drive mechanism 23 thereof, flywheel 22, thruster 21, storage tank 26, antenna 25, moving parts such as magnetic levitation...

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Abstract

The invention provides a dual-super-satellite platform load cabin compound control method. The method includes the following steps that firstly, the attitude of a load cabin is controlled; secondly, the attitude of a platform cabin is controlled; thirdly, the relative positions of the platform cabin and the load cabin are adjusted; and fourthly, according to attitude information of the load cabin,the attitude control system bandwidth of the load cabin is adjusted, and the attitude of the load cabin is restrained. The method has the beneficial effects that through dual-super-platform master and slave cooperative control, load cabin interference compensation control and a variable bandwidth control method, the steady state time of the load cabin is prolonged, and the steady state accuracy of the load cabin is improved.

Description

technical field [0001] The invention relates to a compound control method for a satellite platform load compartment with ultra-high pointing accuracy and ultra-high stability (double super), the platform adopts the active control of the load compartment, the slave control of the platform compartment, and the control method of coordinated decoupling of the two compartments . When the two cabins are initially unlocked in orbit, in order to overcome the impact interference of unlocking, the load cabin adopts high-bandwidth control to make its attitude converge rapidly. control. The load compartment adopts a composite control method, which can improve the attitude stabilization time and stabilization accuracy, and meet the needs of high-precision ground remote sensing. Background technique [0002] The requirements for attitude pointing accuracy and stability of advanced spacecraft in the future are two orders of magnitude higher than the current level, and the dual supersessi...

Claims

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Application Information

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IPC IPC(8): B64G1/24B64G1/28B64G1/36
CPCB64G1/24B64G1/361B64G1/245B64G1/369
Inventor 赵洪波廖鹤唐忠兴朱敏徐毅赵艳彬裘俊邓成晨
Owner SHANGHAI SATELLITE ENG INST
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