LIU Bo, YE Dong, CHE Ren-sheng. Calibration equipment for rocket nozzle motion testing and its error analysis[J]. Editorial Office of Optics and Precision Engineering, 2009,17(7): 1553-1560
LIU Bo, YE Dong, CHE Ren-sheng. Calibration equipment for rocket nozzle motion testing and its error analysis[J]. Editorial Office of Optics and Precision Engineering, 2009,17(7): 1553-1560DOI:
Calibration equipment for rocket nozzle motion testing and its error analysis
The 3D motion parameter measurement of a rocket motor nozzle is a premiss for accurately controlling the nozzle
and the calibration equipment is the key to ensure motion testing at a high precision.To test accurately 3D motion parameters
this paper proposes a new calibration equipment to directly simulate the actual motion of the rocket motor nozzle and to supply the standard position and motion parameters for static and dynamic calibrations. After analyzing the motion of the rocket motor nozzle
a new mechanism consisting of a base
a lifting table
a swing table and a standard nozzle model is proposed
which concludes three degrees of freedom
rotation on
X
and
Y
coordinate axes
lifting on
Z
coordinate axis. The terminal error expression is derived by the theory of multi-system kinematic error in consideration of the geometric errors effect on pointing errors and nozzle center position errors
then the origin of geometric errors is analyzed. By the simulated results
the distribution states of pointing errors and center position errors in rotation ranges are obtained. On the basis of the obtained results
it suggests that the orthogonality errors mostly influncing pointing errors should be controlled below 15
and the axis intersection errors mostly influncing center position errors should be controlled below 80 m.
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references
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