Development of Flight Control System for Automatic Landing Flight Experiment `ALFLEX'

Shigeru Asai, Takashi Hata, Hiroyuki Onuma, Yoshikazu Miyazawa, Tatsushi Izumi

研究成果: Chapter in Book/Report/Conference proceedingOther chapter contribution

抄録

In the extensive development of the H-II Orbiting Plane (HOPE), ALFLEX (Automatic Landing Flight Experiment) was carried out to develop fundamental technologies for a completely autonomous landing for Japan's first unmanned reentry vehicle. National Aerospace Laboratory (NAL), National Space Development Agency of Japan (NASDA) and several manufacturing companies worked together as a unified team and conducted various ground tests and hanging flight tests since March 1996 at Woomera Airfield in South Australia. In July, the first automatic landing test was performed successfully, and in August entire 13 flight tests were completed with outstanding results. As well as these flight test results, this paper outlines the Flight Control System; which performed essential and important roles in ALFLEX, developed by Mitsubishi Heavy Industries, Ltd.

本文言語英語
ホスト出版物のタイトルTechnical Review - Mitsubishi Heavy Industries
出版社Mitsubishi Heavy Industries
ページ125-128
ページ数4
34
3
出版ステータス出版済み - 1997
外部発表はい

All Science Journal Classification (ASJC) codes

  • Mechanical Engineering

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