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Dynamic Inversion via State Dependent Riccati Equation Approach: Application to Flight Vehicles

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. date:
2003
Vol.:
v. 1
Serial:
2003-5361
Paper no.:
AIAA-2003-5361
Page(from):
430
Page(to):
438
Pages:
9
Pub. info.:
Reston, Va.: American Institute of Aeronautics and Astronautics
ISBN:
9781563476020 [1563476029]
Language:
English
Call no.:
A07400/035321 (v.1)
Type:
Technical Paper

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