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The integration of the various EAPS with the helicopter system are discussed.
This paper addresses the problem of designing a robust control for a laboratory 3DOF helicopter system.
Finally, simulation results for CE150 helicopter system illustrate the effectiveness of the proposed approaches.
The effectiveness of this technique is shown for a real-time experimental laboratory-scale helicopter system.
This paper focuses on designing control laws for two-degree of freedom helicopter system while assuring the closed-loop stability.
The unmanned helicopter system is capable of achieving the desired performance in accordance with the military standard under examination.
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This study proposes a solution to the problem of designing adaptive global sliding mode controllers for a class of linear helicopter systems with actuator faults and time delay.
The application of this new approach has been applied successfully in the 3 DOF helicopter systems, showing the effectiveness and potential of the proposed design techniques.
We present in the paper the design of a hardware-in-the-loop simulation framework and its actual implementation on our custom constructed unmanned-aerial-vehicle (UAV) helicopter systems.
The Kolkata class share similar dimensions to the previous Delhi class, however they have 2,363 modifications which include major upgrades in weaponry, sensors and helicopter systems.
In order to develop an efficient helicopter TEM system, it is necessary to analyze and optimize the system parameters.
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