Optimal ascent trajectory and guidance law for aerospace plane

Optimal ascent trajectory and guidance law for aerospace plane

Author(s):

Suzuki, H. ( National Aerospace Laboratory, Japan )
Fushimi, H. ( Kaganawa, Japan )
Matsumoto, Y. ( Mitsubishi Space Software, Co., Japan )
Kimura, S. ( Ishikawajima-Harima Heavy Industries Co., Japan )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1999

Pub. Year:

1999

No.:

99-0386

Paper no.:

99-0386

Page(from):

1

Page(to):

9

Pages:

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050873
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1999.01.11-1999.01.14
Note for article:	37th AIAA Aerospace Sciences Meeting and Exhibit, January 11-14, 1999/Reno, NV

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