Takeoff and Landing Robust Control System for a Tandem Canard Uav-Reference-Cited by-同舟云学术

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Takeoff and Landing Robust Control System for a Tandem Canard Uav

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Alonge A.¹,D'Ippolito Filippo¹,Grillo Caterina¹

Affiliation:

1. University of Palermo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3447

Reference11 articles.

1. Aerodynamic design assessment of Strato 2C and its potential for unmanned high altitude airborne platforms

2. 2Nelson,R.C.,FlightStabilityandAutomaticControl,McGraw-HillBookCompany,NewYork,1989.

3. 3Stevens,B.L.,LewisF.L.,AircraftControlandSimulation,JohnWiley&Sons,Inc.,New York,1992.

4. 4BlakelockJ.H.,AutomaticcontrolofAircraft&Missiles,JohnWiley&Sons,Inc.,New York,1992.

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2. A Model Aided Inertial Navigation System for Automatic Landing of Unmanned Aerial Vehicles;Navigation;2018-06

3. Anti-crosswind Autolanding of UAVs based on Active Disturbance Rejection Control;AIAA Guidance, Navigation, and Control Conference;2010-06-26

4. State Estimation of a Nonlinear Unmanned Aerial Vehicle Model using an Extended Kalman Filter;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28

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