Index Approach Law Based Sliding Control for a Hypersonic Aircraft

Index Approach Law Based Sliding Control for a Hypersonic Aircraft

Author(s):

H. Li ( Beihang University, Beijing, China (prc) )
W. Sun
Z. Li
S. Xue

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : U.S. Air Force T&E Days

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-1734

Paper no.:

AIAA Paper 2009-1734

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200902

Type:

Technical Paper

Details

TDL ID:	ZA00011780
Series ID:	PA00000047
Conf. info. (Name):	U.S. Air Force T&E Days 2009
Conf. info. (Number):	2009
Conf. info. (Venue):	Albuquerque, NM, USA
Conf. info. (Date):	2009.02.10-2009..02.12
Note for article:	U.S. Air Force T&E Days 2009, 10-12 February 2009, Albuquerque, New Mexico

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