Error Compensation Method for Large Complex Electromechanical System
A technology of electromechanical system and error compensation, applied in the direction of control/regulation system, non-electric variable control, position/direction control, etc.
Inactive Publication Date: 2014-06-18
ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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Problems solved by technology
Conventional design techniques cannot meet the requirements of mechanical and electrical equipment, and some compensation strategies must be arranged reasonably
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[0057]
[0072] B:=F001-F000;
[0073] C:=F010-F000;
[0081] In summary, the above are only preferred embodiments of the present invention, and are not intended to limit the scope of protection of the present invention.
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The invention discloses a large-scale complex electromechanical system error compensation method. First, 6 force application points are arranged, and the angle of each 2 force application points is 60 degrees. Every 3 force application points form a group, and the two groups of force application points are symmetrically arranged on the surface of the moon. Both sides of the broadside of the simulation field; the measurement space of 16 meters in length, 16 meters in width and 80 meters in height is divided into n feature points according to the measurement of 1 meter, and error compensation is carried out on feature points and non-feature points. The complex electromechanical system performs error compensation, which makes the system more accurate and better in operation.
Description
Large complex electromechanical system error compensation method Technical field [0001] The present invention relates to a large complex electromechanical system error compensation method, which belongs to the field of aerospace exploration and design. Background technique The moon is 38,000 kilometers away from the earth, but the first-phase lunar exploration project has been used as the basis, and the key of the whole second-phase lunar project It is reflected in the word "soft", to achieve a soft landing, to land the lunar probe on the surface of the moon, instead of sending the lunar probe directly on the surface of the moon. However, the surface of the moon does not have an atmosphere like that of the earth, and it can use landings like the "Shenzhou spacecraft" to Parachute to slow the descent of the lunar probe. Therefore, it is necessary to use technology like that used in rockets, using the recoil of the engine to slow down the descent of the lunar probe. ...
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IPC IPC(8): G05D1/00
Inventor 董强王晓明吴涧彤方志刚陆乐孙宪旺郭华陈强杨永魁王媛丽
Owner ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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