Flight control system for the automatic landing flight experiment

Yoshikazu Miyazawa, Kazutoshi Ishikawa, Toshikazu Motoda, Tatsushi Izumi, Masakazu Sagisaka, Takashi Hata, Hiroyuki Onuma

Research output: Contribution to conferencePaper

3 Citations (Scopus)

Abstract

This paper discusses the flight control system developed for the Automatic Landing FLight Experiment, ALFLEX. ALFLEX is an experimental program conducted by the National Aerospace Laboratory and the National Space Development Agency of Japan in order to investigate the automatic landing technology for a future unmanned reentry space vehicle. The ALFLEX vehicle is a dynamically similar sub-scale model of the planned Japanese HII Orbiting Plane, HOPE. Since the HOPE program is in a preliminary conceptual design phase, the ALFLEX vehicle is a scaled model of one of the proposed configurations from 1992 research. The vehicle bare airframe is statically unstable in the pitch axis. In the lateral-directional axes, it has negative weather cock stability and strong dihedral effect, which introduce severe instability. The airframe's instability and the landing performance requirement drive the flight control system design to be one of the key technologies in the HOPE program. Since the vehicle's maximum L/D is approximately 4, it needs the same landing guidance technique as lifting body research vehicles and the Space Shuttle. This paper discusses the flight control design and the design methods applied to ALFLEX, and discusses lessons learned so far. The results from a preliminary flight test are briefly introduced. The series of automatic landing flights are scheduled for the middle of 1996, at Woomera, Australia, and will verify the guidance, navigation and control design.

Original languageEnglish
Pages1-10
Number of pages10
Publication statusPublished - Jan 1 1996
EventGuidance, Navigation, and Control Conference and Exhibit, 1996 - San Diego, United States
Duration: Jul 29 1996Jul 31 1996

Other

OtherGuidance, Navigation, and Control Conference and Exhibit, 1996
CountryUnited States
CitySan Diego
Period7/29/967/31/96

Fingerprint

Flight control systems
Landing
Airframes
Experiments
Reentry
Space shuttles
Conceptual design
Navigation
Systems analysis

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Aerospace Engineering

Cite this

Miyazawa, Y., Ishikawa, K., Motoda, T., Izumi, T., Sagisaka, M., Hata, T., & Onuma, H. (1996). Flight control system for the automatic landing flight experiment. 1-10. Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1996, San Diego, United States.

Flight control system for the automatic landing flight experiment. / Miyazawa, Yoshikazu; Ishikawa, Kazutoshi; Motoda, Toshikazu; Izumi, Tatsushi; Sagisaka, Masakazu; Hata, Takashi; Onuma, Hiroyuki.

1996. 1-10 Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1996, San Diego, United States.

Research output: Contribution to conferencePaper

Miyazawa, Y, Ishikawa, K, Motoda, T, Izumi, T, Sagisaka, M, Hata, T & Onuma, H 1996, 'Flight control system for the automatic landing flight experiment' Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1996, San Diego, United States, 7/29/96 - 7/31/96, pp. 1-10.
Miyazawa Y, Ishikawa K, Motoda T, Izumi T, Sagisaka M, Hata T et al. Flight control system for the automatic landing flight experiment. 1996. Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1996, San Diego, United States.
Miyazawa, Yoshikazu ; Ishikawa, Kazutoshi ; Motoda, Toshikazu ; Izumi, Tatsushi ; Sagisaka, Masakazu ; Hata, Takashi ; Onuma, Hiroyuki. / Flight control system for the automatic landing flight experiment. Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1996, San Diego, United States.10 p.
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