Blank Cover Image

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. Year:
2003
Vol.:
v. 1
No.:
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

Similar Items:

Shankar, P., Yedavalli, R., Doman, D.

American Institute of Aeronautics and Astronautics

A. Verma, P. Xu, K. Vadakkeveedu, R. Mayer, M. Oppenheimer, D. Doman

American Institute of Aeronautics and Astronautics

Bogdanov, A., Carlsson, M., Harvey, G., Hunt, J., Kieburtz, D., Van der Merwe, R., Wan, E.

American Institute of Aeronautics and Astronautics

Doman,D.

American Institute of Aeronautics and Astronautics

P. Shankar, R. Yedavalli, J. Burken

American Institute of Aeronautics and Astronautics

T. Adami, J. Zhu, M. Bolender, D. Doman, M. Oppenheimer

American Institute of Aeronautics and Astronautics

Mracek, Curtis P., Cloutier, James R.

American Institute of Aeronautics and Astronautics

Yedavalli, R., Shankar, P., Siddiqi, M., Behbahani, A.

American Institute of Aeronautics and Astronautics

Yedavalli, R.

American Institute of Aeronautics and Astronautics

Shankar, P., Yedavalli, R.K.

American Society of Mechanical Engineers

Smith, P.R.

American Institute of Aeronautics and Astronautics

Yedavalli, R.K.

National Aeronautics and Space Administration

1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12