Blank Cover Image

Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method

Author(s):
  • Mracek, Curtis P. ( Navigation and Control Branch, U.S. Air Force Armament Directorate )
  • Cloutier, James R. ( Navigation and Control Branch, U.S. Air Force Armament Directorate )
Publication title:
A collection of technical papers : AIAA Guidance, Navigation and Control Conference, August 11-13, 1997, New Orleans, LA
Title of ser.:
AIAA Paper : AIAA Guidance Navigation and Control Conference
Ser. no.:
CP9710
Pub. Year:
1997
Vol.:
Pt. 3
No.:
97-3767
Paper no.:
AIAA-97-3767
Page(from):
1697
Page(to):
1705
Pub. info.:
Reston, VA: American Institute of Aeronautics and Astronautics
ISBN:
9781563472343 [1563472341]
Language:
English
Call no.:
(pt.1)A07400/9710-1,(pt.2)A07400/9710-2,(pt.3)A07400/9710-3
Type:
Technical Paper

Similar Items:

1 Technical Paper Missile Longitudinal Autopilots: Connections Between Optimal Control and Classical Topologies

Mracek, C., Ridgely, D.

American Institute of Aeronautics and Astronautics
7 Technical Paper Periodically preconditioned conjugate gradient restoration algorithm for optimal control - the direct approach

Mracek, Curtis, Cloutier, James, D'Souza, Chris

American Institute of Aeronautics and Astronautics
2 Technical Paper Missile Longitudinal Autopilots: Comparison of Multiple Three Loop Topologies

Mracek, C., Ridgely, D.

American Institute of Aeronautics and Astronautics
8 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
3 Technical Paper Nonlinear Control Using the State Dependent Coefficient Pole Placement Technique

C. Mracek

American Institute of Aeronautics and Astronautics
9 Technical Paper State-Dependent Riccati Equation Control of a Small Unmanned Helicopter

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

American Institute of Aeronautics and Astronautics
4 Technical Paper Dynamic Inversion via State Dependent Riccati Equation Approach: Application to Flight Vehicles

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

American Institute of Aeronautics and Astronautics
10 Technical Paper L1 Adaptive Controller for a Missile longitudinal Autopilot Design

J. Wang, C. Cao, N. Hovakimyan, R. Hindman, D. Ridgely

American Institute of Aeronautics and Astronautics
5 Technical Paper Autopilot Design for a Missile with Reaction-Jet Using Coefficient Diagram Method

Hirokawa,R., Sato,K., Manabe,S.

American Institute of Aeronautics and Astronautics
11 Technical Paper Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method.

Xin, M., Balakrishnan, S.N.

American Institute of Aeronautics and Astronautics
6 Technical Paper "Nonlinear, Hybrid Bank-to-Turn/Skid-to-Turn Missile Autopilot Design"

Cloutier,J., Stansbery,D.

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