Blank Cover Image

Autopilot Design for a Missile with Reaction-Jet Using Coefficient Diagram Method

Author(s):
Publication title:
A collection of technical papers : AIAA Guidance, Navigation and Control Conference, Montreal, Canada 6-9 August 2001
Title of ser.:
AIAA Paper : AIAA Guidance Navigation and Control Conference
Ser. no.:
2001
Pub. Year:
2001
Vol.:
Pt. 2
No.:
2001-4162
Paper no.:
AIAA-2001-4162
Page(from):
739
Page(to):
746
Pages:
8
Pub. info.:
Reston, VA: American Institute of Aeronautics and Astronautics
ISBN:
9781563474835 [1563474832]
Language:
English
Call no.:
A07400/014018
Type:
Technical Paper

Similar Items:

1 Technical Paper Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method.

Xin, M., Balakrishnan, S.N.

American Institute of Aeronautics and Astronautics
7 Technical Paper Optimal Terminal Trajectories for Clutter Crossover Avoidance of a Variable Flow Ducted Rocket Missile

Kuroda,T., Hirokawa,R., Matsuda,H., Okamoto,K., Mihara,S., Imado,F.

American Institute of Aeronautics and Astronautics
2 Technical Paper Nonlinear missile autopilot design using time-scale separation

Menou, P.K., Iragavarapu, V.R., Ohlmeyer, E.J.

American Institute of Aeronautics and Astronautics
8 Technical Paper Missile Longitudinal Autopilot Design Using a New Model Following Robust Neuro-Adaptive Controller

Unnikrishnan, N., Balakrishnan, S.

American Institute of Aeronautics and Astronautics
3 Technical Paper Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method

Mracek, Curtis P., Cloutier, James R.

American Institute of Aeronautics and Astronautics
9 Technical Paper ADVANCED CONTROL FOR THE DESIGN OF STT MISSILE AUTOPILOT.

BENDOTTI, R.

National Aeronautics and Space Adminstration
4 Technical Paper A Trade Study On Missile Autopilot Design Using Optimal Control Theory

K. Wise

American Institute of Aeronautics and Astronautics
10 Technical Paper Predictive Estimation and Control Based Missile Autopilot Design

Talole, S., Upreti, V., Phadke, S.

American Institute of Aeronautics and Astronautics
5 Technical Paper Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation

McLain,T., Beard,R.

American Institute of Aeronautics and Astronautics
11 Technical Paper Autopilot Design for a Square Cross-section Missile

Hyde, R., Cleminson, J.

American Institute of Aeronautics and Astronautics
6 Technical Paper BANK-TO- TURN MISSILES AND AUTOPILOT DESIGN

KNILL RAF, T S , Flight Lieutenant, Forsythe W , Dr phD MSc BSc, Lewis-Morris, M J , Flt Lt MSc BSc RAF

National Aeronautics and Space Adminstration
12 Technical Paper Design of nonlinear autopilots for high angle of attack missiles

Menon, P.K., Yousefpor, M.

American Institute of Aeronautics and Astronautics
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12