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METHOD OF MAPPING THE CELESTIAL SPHERE AND SPACECRAFT FOR ITS REALIZATION

机译:映射球状体和航天器以实现的方法

摘要

FIELD: space engineering. SUBSTANCE: method of mapping includes the survey of the celestial sphere from aboard spacecraft 3 by way of scanning ring zones 10 by astronomical telescope with two observation tubes 4,5. One observation tube 4 is oriented on reference star 8. Spacecraft 3 is rotated relative to this direction till they penetrate into the field of vision of the other observation tube 5 of measured star 9, star pictures are stabilized on the focal plane, linear distances between their projections are measured and the angle between reference 8 and measured 9 stars is determined, the star pictures are stabilized on the focal plane, the linear distances between their projections are measured and the angle between reference 8 and measured 9 stars is determined. Then the rotation of the spacecraft relative to the reference point is resumed and the angles between reference star 9 and other measured stars are determined. Then they proceed to the scan of the next ring zone 10 by means of reorientation of spacecraft 3 on another reference star 9. Spacecraft 3 for mapping the celestial sphere contains hard-mounted on its housing astrometrical telescope with two observation tubes 4,5 located at the angle of 85-95 degrees to each other and optically conjugated through two flat hard-mounted mirrors with an objective made according to Cassegrain diagram. A flat mirror is mounted on the objective optical axis. A flat mirror operable by a unit of picture precision stabilization is mounted at an angle to the objective axis. The unit input is connected to a photodetector made in the form of matrix of charge-coupled devices. Solar-cell panels and the radiator-cooler of the thermal-regulation system are located on different sides of spacecraft 3 parallel to its longitudinal axis and to each other. The radiator-cooler is fastened to the spacecraft housing from the side of reference observation tube 4. EFFECT: enhanced efficiency and output of astronomical measurements from the cosmos under the conditions of mass-power limitations. 3 cl, 3 dwg
机译:领域:空间工程。实质:测绘方法包括通过带有两个观察管4,5的天文望远镜扫描环带10来测量航天器3上的天球。一个观测管4对准参考恒星8。航天器3相对于该方向旋转,直到它们进入被测恒星9的另一个观测管5的视野内,恒星图像稳定在焦平面上,两者之间的线性距离稳定。测量它们的投影并确定参考8星和9个星之间的角度,将恒星图像稳定在焦平面上,测量其投影之间的线性距离,并确定参考8星和9个星之间的角度。然后,恢复航天器相对于参考点的旋转,并确定参考星9与其他测量星之间的角度。然后,他们通过在另一颗参考星9上重新调整航天器3的位置,对下一个环形区10进行扫描。用于绘制天体图的航天器3硬安装在其外壳的天文望远镜上,其两个观测管4,5位于彼此成85-95度的角度,并通过两个平坦的硬安装镜光学共轭,并根据卡塞格伦图制作了一个物镜。平面镜安装在物镜光轴上。可通过图像精度稳定单元操作的平面镜与物镜轴成一定角度安装。单元输入连接到以电荷耦合器件矩阵形式制成的光电检测器。热调节系统的太阳能电池板和散热器冷却器平行于航天器3的纵轴并彼此平行地位于航天器3的不同侧。散热器冷却器从参考观察管4的一侧固定到航天器的外壳上。效果:在质量功率受限的情况下,效率提高了,宇宙的天文测量结果也有所提高。 3 cl,3 dwg

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