PROBLEM TO BE SOLVED: To provide a simply configured alignment device that can adjust the alignment of a space missile while in flight.SOLUTION: An alignment device is equipped with a base part 11b installed in a missile; a loading part 11a to be loaded with optical system equipment 7; an optical bench 11 provided with a plurality of legs 11c erected on the base part and supporting the loading part; heaters 12 fitted to the plurality of legs to heat the legs; a displacement measuring unit 13 that measures the inclination of the loading part relative to the base part and outputs the result as measurement information; and an alignment control section 14 that calculates the conditions of electrifying the plurality of heaters and so controls the electrification as to keep within a prescribed range the difference between the measurement information and alignment adjustment information inputted from outside indicating the quantity of aligning the loading part relative to the base part.SELECTED DRAWING: Figure 1

    【課題】簡単な構成で、宇宙飛翔体の飛翔中にアライメント調整ができるアライメント装置を提供する。【解決手段】飛翔体に設置されるベース部11b、光学系機器7が搭載される搭載部11a、及び、ベース部に立設されて、搭載部を支持する複数の脚部11cを備える光学ベンチ11と、複数の脚部に取り付けられて、脚部を加熱する加熱器12と、ベース部に対する搭載部の傾きを計測して計測情報として出力する変位計測部13と、計測情報と、外部から入力するベース部に対する搭載部のアライメント量を示すアライメント調整情報との差分が所定範囲に収まるように、複数の加熱器への通電条件を演算して通電制御するアライメント制御部14と、を備える。【選択図】図1


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    Title :

    ALIGNMENT DEVICE FOR SPACE MISSILES


    Additional title:

    宇宙飛翔体のアライメント装置


    Contributors:

    Publication date :

    2016-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / B64G Raumfahrt , COSMONAUTICS



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