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A Concept of the Terminal Descent Control Algorithm at Reentry into the Earth Atmosphere with Near-Parabolic Velocity

机译:接近抛物线速度的进入地球大气层的终端下降控制算法的概念

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摘要

A concept of the terminal descent control algorithm of the descent module at reentry into the Earth atmosphere with near-parabolic velocity is proposed. Trajectories with one and two (skip reentry) reentries are considered. Simultaneously, downrange and crossrange misses are eliminated by controlling the bank angle and time of bank angle reversal at each phase of the trajectory. The designed control meets the specified load factor constraint.
机译:提出了以近抛物线速度折返地球大气层的下降模块终端下降控制算法的概念。考虑具有一次和两次(跳过折返)折返的轨迹。同时,通过控制轨迹的每个相位的倾斜角和倾斜角反转的时间,可以消除下距和跨范围遗漏。设计的控件满足指定的负载因子约束。

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    Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia S.P. Korolev Rocket and Space Corporation Energia, ul. Lenina 4a, Korolev, Moscow oblast, Russia;

    Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia S.P. Korolev Rocket and Space Corporation Energia, ul. Lenina 4a, Korolev, Moscow oblast, Russia;

    Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia S.P. Korolev Rocket and Space Corporation Energia, ul. Lenina 4a, Korolev, Moscow oblast, Russia;

    Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia S.P. Korolev Rocket and Space Corporation Energia, ul. Lenina 4a, Korolev, Moscow oblast, Russia;

    Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia S.P. Korolev Rocket and Space Corporation Energia, ul. Lenina 4a, Korolev, Moscow oblast, Russia;

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