首页> 外国专利> METHOD OF FORMING CONTROL MOMENTS FOR SPACE VEHICLE WITH MAGNETOINERTIAL ACTUATORS, SYSTEM OF FORMING CONTROL MOMENTS FOR SPACE VEHICLE WITH MAGNETOINERTIAL ACTUATORS AND MAGNETOINERTIAL ACTUATOR

METHOD OF FORMING CONTROL MOMENTS FOR SPACE VEHICLE WITH MAGNETOINERTIAL ACTUATORS, SYSTEM OF FORMING CONTROL MOMENTS FOR SPACE VEHICLE WITH MAGNETOINERTIAL ACTUATORS AND MAGNETOINERTIAL ACTUATOR

机译:用磁动致动器形成空间控制力矩的方法,用磁动致动器形成空间力矩的控制系统和磁动致动器

摘要

FIELD: space engineering. SUBSTANCE: magnetic and gravitational control moments are formed on board of space vehicle by acting magnetically on sedimentary stable highly concentrated magnetorheological fluid. Highly concentrated magnetorheological fluid used as dampening medium enhances efficiency of dampening process due to increased coefficient of dampening at fixed structural, inertial and mass characteristics of the damper, as well as due to maintenance of maximum magnitude of dampening coefficient in course of dampening at magnetothermal transfer of cooled highly concentrated magnetorheological fluid to zone of intensive heating of fluid. After shifting to mode of control of angular motion of space vehicle, actions pertaining to directional magnetizing of highly concentrated magnetorheological fluid till permanent magnet is obtained and control of this magnet make it possible to attain high efficiency in control of space vehicle due to increase of absolute magnitude of total control moment (gravitational + magnetic). Increase of magnitude of gravitational moment is achieved through directional redistribution of mass of fluid by changing its density. In course of control, discrepancy in requirements for application of magnetic and gravitational control moments is eliminated. Since highly concentrated magnetizing/demagnetizing, changes from modes of dampening to mode of control of angular motion of space vehicle and vice versa may be unlimitedly cycled. System for realizing the above method in addition to standard sensors of angular velocity, unit for forming required control moments, three-channel magnetometer, unit for setting the parameters of space vehicle and modes of orientation includes some units and devices for performing the actions stipulated by the method, viz.: magnetoinertial actuator on base of highly concentrated magnetorheological fluid, unit for forming the corrections for kinematic circuit of control of magnetoinertial element, unit for shaping the control signals, unit for forming dampening element, unit for forming magnetoinertial element and unit for forming control magnetic fields. Functional interconnection of units of the system makes it possible to achieve the required results of the method. Main part of system is new magnetoinertial actuator on base of highly concentrated magnetorheological fluid. This actuator consists of hollow spherical housing made of nonmagnetic material and filled with highly concentrated magnetorheological fluid, fluid compensator, two bypass valves, two connecting pipes ("hot" and "cold" fluid), cooler, two electromagnets, casing-magnetic circuit, three pairs of commutatorless electric motors arranged along axes of control of device OX, OY, OZ, three sensors for measurement of speed of relative linear motion of spherical housing of device OX, OY, OZ, two-degree-of-freedom electrical mechanical retainer of device housing. EFFECT: enhanced efficiency. 4 cl, 12 dwg
机译:领域:空间工程。物质:磁性和重力控制力矩是通过磁性作用于沉积稳定的高浓度磁流变流体而在航天器板上形成的。由于阻尼器在固定结构,惯性和质量特性下的阻尼系数增加,以及在磁热传递过程中保持阻尼系数的最大幅度,因此,用作阻尼介质的高浓度磁流变液可提高阻尼过程的效率。冷却的高浓度磁流变流体到流体强烈加热的区域。转变为航天器角向运动的控制方式后,与获得高度浓缩的磁流变流体的定向磁化直到获得永磁体有关的动作,并且该磁体的控制使得由于绝对值的增加而可以实现航天器的高效控制。总控制力矩的大小(重力+磁场)。通过改变流体的密度通过定向流体质量的重新分配,可以增加重力矩的大小。在控制过程中,消除了施加磁矩和重力控制力矩的要求方面的差异。由于高度集中的磁化/消磁,所以可以无限地循环从阻尼模式到空间飞行器的角运动控制模式的变化,反之亦然。除了标准的角速度传感器,用于形成所需控制力矩的单元,三通道磁力计,用于设置航天器参数和定向方式的单元以外,用于实现上述方法的系统还包括一些单元和执行以下操作的装置:该方法,即:基于高度集中的磁流变流体的磁电致动器,用于形成磁电元件控制运动学校正的单元,用于成形控制信号的单元,用于形成阻尼元件的单元,用于形成磁电元件的单元和单元用于形成控制磁场。系统单元的功能互连使实现该方法所需的结果成为可能。系统的主要部分是基于高浓度磁流变流体的新型磁电致动器。该执行器由非磁性材料制成的空心球形外壳组成,并填充有高浓度的磁流变流体,流体补偿器,两个旁通阀,两个连接管(“热”和“冷”流体),冷却器,两个电磁体,外壳磁路,沿设备OX,OY,OZ的控制轴排列的三对无换向器电动机,三个用于测量设备OX,OY,OZ的球形外壳的相对线性运动速度的传感器,两自由度机电固定器设备外壳。效果:提高效率。 4厘升,12载重吨

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