Alflex flight simulation analysis and flight testing

Toshikazu Motoda; Yoshikazu Miyazawa; Kazutoshi Ishikawa; Tatsushi Izumi

Alflex flight simulation analysis and flight testing

Toshikazu Motoda, Yoshikazu Miyazawa, Kazutoshi Ishikawa, Tatsushi Izumi

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

The Automatic Landing Flight Experiment (ALFLEX) was conducted in Woomera, Australia, in 1996 in order to develop the automatic landing technology required for the future Japanese unmanned spacecraft, HOPE. In order to ensure successful landings, computer simulation played an important role in the preflight analysis. Monte Carlo Simulation was applied for the analysis. The Root Sum Square (RSS) method, which is commonly used in Japanese launcher rocket development projects, was also applied. Monte Carlo results were compared with the RSS results and the flight test results. All 13 flighttests were successfully completed. Longitudinal guidance in the flare phase was found to be sensitive to some modeling-errors. The cause is discussed.

Original language	English
Title of host publication	36th AIAA Aerospace Sciences Meeting and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
Publication status	Published - 1998
Externally published	Yes
Event	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States Duration: Jan 12 1998 → Jan 15 1998

Other

Other	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998
Country/Territory	United States
City	Reno
Period	1/12/98 → 1/15/98

All Science Journal Classification (ASJC) codes

Engineering(all)
Space and Planetary Science

Cite this

@inproceedings{daaf89f816ae4f1cb8d88946ce30e642,

title = "Alflex flight simulation analysis and flight testing",

abstract = "The Automatic Landing Flight Experiment (ALFLEX) was conducted in Woomera, Australia, in 1996 in order to develop the automatic landing technology required for the future Japanese unmanned spacecraft, HOPE. In order to ensure successful landings, computer simulation played an important role in the preflight analysis. Monte Carlo Simulation was applied for the analysis. The Root Sum Square (RSS) method, which is commonly used in Japanese launcher rocket development projects, was also applied. Monte Carlo results were compared with the RSS results and the flight test results. All 13 flighttests were successfully completed. Longitudinal guidance in the flare phase was found to be sensitive to some modeling-errors. The cause is discussed.",

author = "Toshikazu Motoda and Yoshikazu Miyazawa and Kazutoshi Ishikawa and Tatsushi Izumi",

year = "1998",

language = "English",

booktitle = "36th AIAA Aerospace Sciences Meeting and Exhibit",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

note = "36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 ; Conference date: 12-01-1998 Through 15-01-1998",

}

TY - GEN

T1 - Alflex flight simulation analysis and flight testing

AU - Motoda, Toshikazu

AU - Miyazawa, Yoshikazu

AU - Ishikawa, Kazutoshi

AU - Izumi, Tatsushi

PY - 1998

Y1 - 1998

N2 - The Automatic Landing Flight Experiment (ALFLEX) was conducted in Woomera, Australia, in 1996 in order to develop the automatic landing technology required for the future Japanese unmanned spacecraft, HOPE. In order to ensure successful landings, computer simulation played an important role in the preflight analysis. Monte Carlo Simulation was applied for the analysis. The Root Sum Square (RSS) method, which is commonly used in Japanese launcher rocket development projects, was also applied. Monte Carlo results were compared with the RSS results and the flight test results. All 13 flighttests were successfully completed. Longitudinal guidance in the flare phase was found to be sensitive to some modeling-errors. The cause is discussed.

AB - The Automatic Landing Flight Experiment (ALFLEX) was conducted in Woomera, Australia, in 1996 in order to develop the automatic landing technology required for the future Japanese unmanned spacecraft, HOPE. In order to ensure successful landings, computer simulation played an important role in the preflight analysis. Monte Carlo Simulation was applied for the analysis. The Root Sum Square (RSS) method, which is commonly used in Japanese launcher rocket development projects, was also applied. Monte Carlo results were compared with the RSS results and the flight test results. All 13 flighttests were successfully completed. Longitudinal guidance in the flare phase was found to be sensitive to some modeling-errors. The cause is discussed.

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UR - http://www.scopus.com/inward/citedby.url?scp=84983122419&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84983122419

BT - 36th AIAA Aerospace Sciences Meeting and Exhibit

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998

Y2 - 11 January 1998 through 14 January 1998

ER -

Alflex flight simulation analysis and flight testing

Abstract

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All Science Journal Classification (ASJC) codes

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