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METHOD OF NAVIGATING SPACECRAFT BASED ON CELESTIAL PERIODIC RADIATION SOURCES

机译:基于卫星周期辐射源的航天器导航方法

摘要

FIELD: physics.;SUBSTANCE: method of navigating spacecraft based on pulsed radiation of pulsars involves determination of a set of intervals of pulses from pulsars independently on on-board and ground-based telescope on a coordinated epoch of observations on set dates, which are then used to correct values of the observed period on the ground-based telescope and deviation of the observed period from the average value on the on-board telescope; the obtained values of the observed period are used to calculate deviation of intervals of pulses from pulsars, observed on the on-board and ground-based telescopes; the difference between deviation of intervals on the on-board and ground-based telescopes is used to determine the radius vector of the true location of the spacecraft relative the calculated trajectory point and vector values of velocity and acceleration of the spacecraft, from which a decision to perform an adjustment manoeuvre to approach the true and calculated trajectory of the spacecraft is made. By associating the location of the spacecraft with the observed intervals of highly stable period radiation of pulsars, high accuracy of determining the vector of navigation state and control of results of performing adjustment manoeuvres of the spacecraft is achieved.;EFFECT: high efficiency of measuring navigation parameters, high accuracy of determining the vector of the current state and controlling results of performing adjustment manoeuvres of the spacecraft based on the observed periodic pulsed radiation from pulsars.;6 cl, 5 dwg
机译:领域:物理学;物质:基于脉冲星脉冲辐射的航天器导航方法包括在机载和地面望远镜上在设定日期的协调观测周期内独立确定脉冲星的脉冲间隔集。然后用于校正地面望远镜上观测周期的值以及观测周期与机载望远镜平均值的偏差;观测周期的所得值用于计算在机载和地面望远镜上观测到的脉冲与脉冲星的间隔偏差;机载望远镜和地面望远镜的间隔偏差之间的差用于确定航天器相对于计算出的轨迹点的真实位置的半径矢量以及航天器的速度和加速度矢量值,从中可以确定进行调整操作以逼近航天器的真实和计算轨迹。通过将航天器的位置与脉冲星高度稳定的周期辐射的观测间隔相关联,可以实现高精度的导航状态矢量确定和对航天器进行调整操作的结果的控制。参数,基于当前状态向量的高精度确定和基于观测到的来自脉冲星的周期性脉冲辐射对航天器进行调整演算的控制结果; 6 cl,5 dwg

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