𝔖 Bobbio Scriptorium

✦ LIBER ✦

Stabilization of a PVTOL Aircraft and an Inertia Wheel Pendulum Using Saturation Technique

✍ Scribed by Ye, Huawen; Wang, Hong; Wang, Haibo

Book ID: 120284618
Publisher: IEEE
Year: 2007
Tongue: English
Weight: 195 KB
Volume: 15
Category: Article
ISSN: 1063-6536
DOI: 10.1109/TCST.2007.899718

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

The Design and Implementation of a Wheel

The Design and Implementation of a Wheeled Inverted Pendulum Using an Adaptive Output Recurrent Cerebellar Model Articulation Controller

✍ Chih-Hui Chiu 📂 Article 📅 2010 🏛 IEEE 🌐 English ⚖ 1003 KB

[IEEE 42nd IEEE International Conference

[IEEE 42nd IEEE International Conference on Decision and Control - Maui, HI, USA (9-12 Dec. 2003)] 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475) - Control strategy using vision for the stabilization of an experimental PVTOL aircraft setup

✍ Palomino, A.; Castillo, P.; Fantoni, I.; Lozano, R.; Pegard, C. 📂 Article 📅 2003 🏛 IEEE ⚖ 400 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics Aircraft Design and Operations Meeting - Baltimore,MD,U.S.A. (23 September 1991 - 25 September 1991)] Aircraft Design and Operations Meeting - Application of LQG/LTR design technique to aircraft stabilization and control using novel feedback parameters

✍ HYNES, MARSHALL; CLARK, JR., JOHN 📂 Article 📅 1991 🏛 American Institute of Aeronautics and Astronautics ⚖ 1019 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics Guidance, Navigation, and Control Conference and Exhibit - Boston,MA,U.S.A. (10 August 1998 - 12 August 1998)] Guidance, Navigation, and Control Conference and Exhibit - Wide-range stabilization of an arm-driven inverted pendulum using linear parameter-varying techniques

✍ Kajiwara, Hiroyuki; Apkarian, Pierre; Gahinet, Pascal 📂 Article 📅 1998 🏛 American Institute of Aeronautics and Astronautics ⚖ 1001 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 33rd Aerospace Sciences Meeting and Exhibit - Reno,NV,U.S.A. (09 January 1995 - 12 January 1995)] 33rd Aerospace Sciences Meeting and Exhibit - An evaluation of aerodynamic prediction methods applied to the XB-70 for use in high speed aircraft stability and control system design

✍ Razgonyaev, Valery; Mason, W 📂 Article 📅 1995 🏛 American Institute of Aeronautics and Astronautics ⚖ 685 KB

An innovative method for estimating the

An innovative method for estimating the roll angle in two-wheeled vehicles is proposed. the roll angle is a crucial variable in the dynamics of two-wheeled vehicles, since it greatly affects the behaviour of the tire-road contact forces. hence, the capability of providing in real time a reliable measure of such quantity allows us to evaluate the dynamic properties of the vehicle and its tyres, and represents the enabling technology for the design of advanced braking, traction and stability control systems. the method proposed is based on a lowcost sensor configuration, suitable for industrial purposes. the validity of the proposed approach is assessed in a multi-body motorbike simulator environment and also on an instrumented test vehicle.

✍ Boniolo, I.; Savaresi, S.M.; Tanelli, M. 📂 Article 📅 2009 🏛 The Institution of Engineering and Technology 🌐 English ⚖ 1001 KB