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公开(公告)号：KR1020130035740A
公开(公告)日：2013-04-09
申请号：KR1020110100250
申请日：2011-09-30
Applicant: 국방과학연구소
Abstract: PURPOSE: A horizontality control method for a launch platform is provided to improve the horizontal accuracy of the launch platform and a vehicle using a multipoint supporting mode and to supplement the structural deformation. CONSTITUTION: A horizontality control method for a launch platform is as follows. Supporting jacks of the launch platform make a landing on the ground(S10). The horizontality of the launch platform is controlled by moving the supporting jacks according to the gradient information of the launch platform outputted from a rear gradient sensor box(S20). The deformation amount of the launch platform is predicted by the output of a front gradient sensor box. In order that the predicted deformation amount is converged within an error range, a front support jack is controlled to compensate the deformation of the launch platform(S30). [Reference numerals] (AA) Start; (BB,DD,HH,GG) No; (CC,EE,II,FF) Yes; (JJ) End; (S10) Landing step; (S11) Driving a supporting jack; (S12) Automatic landing completed?; (S20) Horizontality controlling step; (S21) Selecting a horizontality reference jack; (S22) Executing horizontality control; (S23) Sensor value
Abstract translation: 目的：提供发射平台的水平控制方法，以提高发射平台和使用多点支持模式的车辆的水平精度，并补充结构变形。 构成：发射平台的水平控制方法如下。 发射平台的支撑插座在地面上着陆（S10）。 通过根据从后梯度传感器箱输出的发射平台的梯度信息移动支撑插座来控制发射平台的水平度（S20）。 发射平台的变形量由前梯度传感器盒的输出预测。 为了将预测的变形量收敛在误差范围内，控制前支撑千斤顶以补偿发射平台的变形（S30）。 （附图标记）（AA）开始; （BB，DD，HH，GG）否; （CC，EE，II，FF）是; （JJ）结束; （S10）着陆步; （S11）驱动支撑千斤顶; （S12）自动着陆完成？ （S20）水平控制步骤; （S21）选择水平参考插孔; （S22）执行水平控制; （S23）传感器值<水平极限？ （S30）变形补偿步骤; （S31）检测发射平台的变形量; （S32，S34）变形量<变形误差？ （S33）操作前支撑插孔;
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