Works matching IS 17568293 AND DT 2013 AND VI 5 AND IP 4
Results: 7
Linear Aerodynamic Model Identification of a Flapping Wing MAV Based on Flight Test Data.
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 273, doi. 10.1260/1756-8293.5.4.273
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- Article
Aerodynamic Characteristics of a Low Aspect Ratio Wing and Propeller Interaction for a Tilt-Body MAV.
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 245, doi. 10.1260/1756-8293.5.4.245
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- Article
Pitch Moment Generation and Measurement in a Robotic Hummingbird.
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 299, doi. 10.1260/1756-8293.5.4.299
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- Article
Special Issue on the International Micro Air Vehicle Conference and Flight Competition 2013 (IMAV 2013).
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. i, doi. 10.1260/1756-8293.5.4.i
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- Article
Development of a Long Endurance Mini-UAV: ETERNITY.
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- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 261, doi. 10.1260/1756-8293.5.4.261
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- Article
An Application of Adaptive Blades on Convertible MAVs.
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 229, doi. 10.1260/1756-8293.5.4.229
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- Article
Optic-flow based slope estimation for autonomous landing.
- Published in:
- International Journal of Micro Air Vehicles, 2013, v. 5, n. 4, p. 287, doi. 10.1260/1756-8293.5.4.287
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- Article