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Featured researches published by Tamiya Nomura.


Acta Astronautica | 1986

Usuda deep space station with 64-meter-diameter antenna

Tamiya Nomura; Tomonao Hayashi; Toshimitsu Nishimura; Haruto Hirosawa; Mitsuru Ichikawa

Abstract Institute of Space and Astronautical Science (ISAS), Japan, constructed a new deep space ground station with 64-meter-diameter antenna at Usuda-cho, Nagano, in 1984. The station has successfully operated in the tracking of “Sakigake”, the first Japanese interplanetary spacecraft that ISAS launched on January 8, 1985. This paper describes the facilities and the features of the Usuda Station, the results of Sakigake tracking, as well as the features of the softwares for trajectory generation and orbit determination that we have developed for deep space missions.


IEEE Transactions on Aerospace and Electronic Systems | 1987

Dual Speed PN Ranging System for Tracking of Deep Space Probes

Zen-icji Yamamoto; Haruto Hirosawa; Tamiya Nomura

A new pseudonoise (PN) ranging system is proposed for trackingof deep space probes, named the dual speed PN ranging system,that transmits two different PN sequences simultaneously through a PSK/PSK (phase-shift keying) dual speed communication channel.The dual speed PN ranging system improves the maximummeasurable range significantly, with no degradation of theacquisition time, when compared with usual PN ranging systems.According to the analysis, the tracking error of this system becomesas small as those of usual PN ranging systems when the inputsignal-to-noise ratio (SNR) is large enough.


Acta Astronautica | 1980

Recent development of scientific satellites and their launch vehicles

Daikichiro Mori; Tamiya Nomura; Tomonao Hayashi; Ryojiro Akiba; Keiken Ninomiya

Abstract The Institute of Space and Aeronautical Science (ISAS), University of Tokyo, has been engaged in the development of scientific satellites and their launch vehicles of Mu series. ISAS has conducted the first flight test of M-3S, the newest version of Mu series, and launched a technology test satellite MS-T4 into an orbit. The objectives were to verify the overall performance of the vehicle and to perform various experiments on the satellite technology to be applied to the following scientific satellites. Technological aspects of M-3S and MS-T4 are reviewed in reference to the recent trend in the scientific satllite program.


Archive | 1985

Communications system for the Japanese interplanetary spacecraft MS-T5/Planet-A

Tamiya Nomura; Tomonao Hayashi; Haruto Hirosawa; Mitsuru Ichikawa; Kouzaburo Inoue


Archive | 1986

Dual speed PN ranging system for deep space exploration

Zen-ichi Yamamoto; Tamiya Nomura; Haruto Hirosawa


Archive | 1986

Design principles of deep space communications equipments of the Usuda Deep Space Center

Tamiya Nomura; Tomonao Hayashi; Haruto Hirosawa; Tadashi Takano; Mitsuru Ichikawa


Archive | 1984

Halley's comet exploration and Usuda's large antenna.

Tamiya Nomura; Tomonao Hayashi; H. Matsuo; Haruto Hirosawa; Mitsuru Ichikawa


Space tracking and data systems; Proceedings of the Symposium | 1981

DEEP SPACE PROJECTS IN JAPAN

Tamiya Nomura; Tomonao Hayashi; Haruto Hirosawa; Keiken Ninomiya; Mitsuru Ichikawa


Archive | 1980

M-3S, A Three-Stage Solid Propellent Rocket for Launching Scientific Satellites

Ryojiro Aklba; Tomonao Hayashi; Daikichiro Mori; Tamiya Nomura


Bulletin of the Institute of Space and Aeronautical Science, University of Tokyo | 1980

Test Satellite "TANSEI-3": MS-T3

Tamiya Nomura; Tomonao Hayashi; Akio Ushirokawa; Keiken Ninomiya; Kozaburo Inoue

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Zen-ichi Yamamoto

Japan Aerospace Exploration Agency

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