Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller

Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller

Author(s):

C. Oh ( Korea Advanced Institute of Science and Technology, Daejeon, South Korea )
H. Bang
J. Park

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Guidance Navigation and Control Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-6182

Paper no.:

AIAA Paper 2006-6182

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200619 [CD-ROM 2006 Disc 19]

Type:

Technical Paper

Details

TDL ID:	ZA00047246
Series ID:	PA00000153
Conf. info. (Name):	AIAA Guidance, Navigation, and Control Conference and Exhibit
Conf. info. (Number):	2006
Conf. info. (Venue):	Keystone, Colorado
Conf. info. (Date):	2006.08.21-2006.08.24

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