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By Adrian Olaru

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Additional resources for Biomechanics, Neurorehabilitation, Mechanical Engineering, Manufacturing Systems, Robotics and Aerospace

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D. adopted for gain/gains in flight ecuations, as trimming parameters within flight test conducted on the couple platform / auto-pilot. 2/Fig3. Uncovered picture during flight tests and modules diagram description of the Spartacus IV auto-pilot. Hardware components /functions: • • • 3 control channels for elevator, aileron and throttle; 6 DOF IMU (solid state gyros): 3 MEMS sensors, 3 accelerometers, 3 channels Kalman filtration gauges; on-board integrated sensors: 3 MEMS sensors, 3 accelerometers, 1 barometric gauge şi 1 Pitot tube, GPS based navigation module; CPU ADI MAG PSA GPS MIX TXR RCM ENG PWM USS REG - central processing unit; atitude (artificial horizont indicator); magnetic module (compass); altitude module, aerodynamic air speed (Pitot); GPS module; mixed command module; communication module (radiomodem); manual control module (Rx – RC external pilot); propulsion monitoring module; battery monitoring module; ultrasonic module (optional); on-board recording parameters (optional).

Introduction The paper presents one assisted method with the proper virtual LabVIEW instruments (VI) for the assisted research of the vibration spectrum of the industrial robots. 2 from National Instruments, USA. Now, in the world, all the dynamic determination of the vibration spectrum are made with the Fourier analyzer apparatus, which it is a special apparatus for these determinations, but the cost of the research is very expensive. 1 and 2). We researched one didactical arm type robot with spring or Fourier spectrum without springs in the second joint.

The sandwich bars are 1 m length. In the Fig. , we have a simplified scheme for the bending of the composite sandwich bar in the first case. We can use the behavior relations from bending calculus of the composite bar. The behavior relations after [2] give: 40 Biomechanics, Neurorehabilitation, Mechanical Engineering, Manufacturing Systems, Robotics and Aerospace x F F F V y V y x x F y v x v l l l ep l ea=et v y M M M F x F b. a. F x c. F x d. Fig. 1. A sandwich composite bar in four cases of buckling.

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