Aircraft control using sliding mode control
- Author(s):
- Tournes, Christian ( The University of Alabama in Huntsville )
- Shtessel, Yuri
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-3692
- Paper no.:
- 96-3692
- Page(from):
- 1
- Page(to):
- 14
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Integrated Guidance and Autopilot for Dual Controlled Missiles Using Higher Order Sliding Mode Controllers and Observers
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Tailless Aircraft Flight Control Using Multiple Time Scale Re-configurable Sliding Modes
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Autopilot for Missiles Steered by Aerodynamic Lift and Divert Thrusters using Nonlinear Dynamic Sliding Manifolds
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Unmanned Rotorcraft Tight Formation Flight Control Using Sliding Mode Control Driven by Sliding Mode Disturbance Observers
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Guidance and Autopilot for Missiles Steered by Aerodynamic Lift and Divert Thrusters Using Second Order Sliding Mode Control
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |