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Titlebook: New Achievements in Unmanned Systems; International Sympos T. Hikmet Karakoc,Nadir Yilmaz,Ali Haydar Ercan Conference proceedings 2023 The

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樓主: 閃爍
51#
發(fā)表于 2025-3-30 08:17:25 | 只看該作者
52#
發(fā)表于 2025-3-30 14:19:57 | 只看該作者
53#
發(fā)表于 2025-3-30 17:36:18 | 只看該作者
Inference of Civil Infrastructure Vibrations Using Unmanned Aerial Vehicles,g technology that makes use of embedded accelerometer data from smartphones and UAVs which is used for bridge acceleration response measurement. This method relies on high landing accuracy and coupling with the structural surface under extreme conditions.
54#
發(fā)表于 2025-3-31 00:00:00 | 只看該作者
55#
發(fā)表于 2025-3-31 02:59:26 | 只看該作者
Nonlinear Six-Degree-of-Freedom Flight Modelling and Trimming of a Single-Propeller Airplane,motion was solved numerically at equilibrium condition for cruising velocity and altitude. Time history variations of all 12 state variables for trimmed flight show instantaneous motion of airplane. The procedure described in this chapter should be useful for the mission evaluation of such a propeller airplane during its preliminary design.
56#
發(fā)表于 2025-3-31 05:12:05 | 只看該作者
Flow Patterns in Double Planar Synthetic Jets, flow patterns with two aims: finding the mechanism triggering the symmetry breaking and to generate a reduced order model, which is interesting for the temporal prediction of the flow, reducing the computational time in the numerical simulations.
57#
發(fā)表于 2025-3-31 12:17:21 | 只看該作者
58#
發(fā)表于 2025-3-31 15:18:23 | 只看該作者
Akan Guven,Chingiz Hajiyevlegungen und operativen Empfehlungen für ein erfolgreiches Crowdfunding. Dazu geh?rt ein ausführliches Portrait der Crowdinvestoren, eine Schritt-für-Schritt-Anleitung des Prozesses sowie zahlreiche Checklisten978-3-658-05925-5978-3-658-05926-2
59#
發(fā)表于 2025-3-31 19:44:14 | 只看該作者
Sam Yoo,Dro Gregorian,Andrew Kopeikin,Nancy Leveson
60#
發(fā)表于 2025-3-31 23:31:46 | 只看該作者
A Test-Bed for Attitude Determination and Control System of Nanosatellite,ol tasks in a distributed control mechanism. Several scenarios are tested and analyzed in the traditional and nontraditional Kalman-type filters for attitude estimation of the satellite and magnetometer calibration purposes.
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