Modeling and Control of a Recoverable Balloon System for Launch of Small Payloads to Low Earth Orbit

Modeling and Control of a Recoverable Balloon System for Launch of Small Payloads to Low Earth Orbit

著者名:

M. Wilson ( Rochester Institute of Technology, Rochester, NY )
A. Crassidis

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-6648

ペーパー番号:

AIAA Paper 2006-6648

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200619 [CD-ROM 2006 Disc 19]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047245
シリーズID:	PA00000162
会議名:	AIAA Atmospheric Flight Mechanics Conference and Exhibit
回次:	2006
会議開催地:	Keystone, Colorado
会議開催年:	2006.08.21-2006.08.24

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5 テクニカルペーパー Tether system for exchanging payloads between low earth orbit and the lunar surface Hoyt, Robert P. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Limit Cycle Oscillation Control of Aeroelastic System Using Model-Error Control Synthesis Kim, J., Crassidis, J. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー A Partially Reusable Launch Vehicle for Delivering 65 Metric Ton Payloads to Low Earth Orbit Donahue, B., Weldon, V., Paris, S. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Electromagnetic Launch to Low Earth Orbit E. Schmidt American Institute of Aeronautics and Astronautics

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