Design and testing of the HOPE-X HSFD-II landing system

Gardinier, Debra; Yanagihara, Masaaki; Kobayashi, Teiu; Amito, Atsushi

doi:10.2514/6.2001-2048

Cited by 3 publications

(2 citation statements)

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“…National Space Development Agency of Japan and National Aerospace Laboratory has developed High Speed Flight Demonstration program (HSFD) [19][20][21][22]. This program is a flight test for research and development of winged re-entry vehicle like HOPE-X.…”

Section: B the Health Management Plan For Hope-x In Japanmentioning

confidence: 99%

Review on integrated health management for aerospace plane

Jinying

2011

Proceedings of 2011 International Conference on Electronic &Amp; Mechanical Engineering and Information Technology

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The references at home and abroad are summarized in this paper. This paper introduces the basic concept and the application significance of aerospace plane, the main differences between the aerospace plane and general aircraft, integrated health management system and its compositions of aerospace plane , the development status of health management for aerospace plane in domestic and foreign countries. Especially it recommends special technical experiments in America, Japan and Italy, and analyzes the health management approaches of them. Finally, it also describes the main fault diagnosis methods. Integrated health management of aerospace plane generally involves a series of activities, including signal processing, monitoring, health assessment, failure prediction, decision support, humancomputer interaction, restoring, and so on. In addition, this paper predicts development direction of health management for the aerospace plane.

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Section: B the Health Management Plan For Hope-x In Japanmentioning

confidence: 99%

Review on integrated health management for aerospace plane

Jinying

2011

Proceedings of 2011 International Conference on Electronic &Amp; Mechanical Engineering and Information Technology

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“…Among the various ways of carrying out supersonic flight experiments, the balloon launch method is one of the most cost-efficient. [6][7][8] While balloon launch is very cost-efficient, it has several limitations. To address them, this paper presents a systematic controller design procedure and a controller design scheme of using the Hierarchy-Structured Dynamic Inversion (HSDI) method, which is based on dynamic inversion (DI) and timescale separation.…”

Section: Introductionmentioning

confidence: 99%

Dynamic Inversion Controller Design for Balloon-Launched Supersonic Aircraft

Ninomiya

Suzuki

Kawaguchi

2018

Trans. Japan Soc. Aero. S Sci.

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While balloon launch is one of the most cost-efficient ways to realize a supersonic flight experiment, it presents some issues for the controller. D-SEND#2 is one flight experiment of this kind which was carried out in 2015. An unpowered test vehicle was lifted to an altitude of 30 km by a balloon and then released. After separation, the vehicle's onboard flight control computer selected a target Boom Measurement System (BMS) according to the separation point. The vehicle then autonomously flew to the BMS selected and established the prescribed sonic boom measurement flight conditions. The design of the guidance, navigation, and control system for the D-SEND#2 flight test was exceptionally challenging, and it was solved by a combination of a sophisticated guidance law and a control law based on dynamic inversion and time scale separation. This paper describes a controller design method for a balloon-launch flight experiment and applied it to a D-SEND#2 control system design. Flight results are presented to show the effectiveness of the controller design method.

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