Dynamic Inversion for Missile Lateral Velocity Control via Polynomial Eigenstructure Assignment

Dynamic Inversion for Missile Lateral Velocity Control via Polynomial Eigenstructure Assignment

Author(s):

Publication title:

A collection of technical papers : AIAA Guidance, Navigation and Control Conference, Austin, Texas, 11-14 August 2003

Title of ser.:

AIAA Paper : AIAA Guidance Navigation and Control Conference

Ser. no.:

2003

Pub. Year:

2003

Vol.:

v. 4

No.:

2003-5792

Paper no.:

AIAA-2003-5792

Page(from):

3066

Page(to):

3072

Pages:

7

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISBN:

9781563476020 [1563476029]

Language:

English

Call no.:

A07400/035321 (v.4)

Type:

Technical Paper

Details

TDL ID:	ZA00001590
Series ID:	PA00000153
Conf. info. (Name):	AIAA Guidance, Navigation and Control Conference
Conf. info. (Number):	2003
Conf. info. (Venue):	Austin, Texas
Conf. info. (Date):	2003.08.11-2003.08.14

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