文件名称:arcs257
- 所属分类:
- 单片机(51,AVR,MSP430等)
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- [PDF]
- 上传时间:
- 2012-11-26
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- 496kb
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- 提 供 者:
- AMIT *****
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SYSTEM MODELLING AND PID CONTROL SYSTEM OF FOUR ROTOR HELICOPTER
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
-SYSTEM MODELLING AND PID CONTROL SYSTEM OF FOUR ROTOR HELICOPTER
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
-SYSTEM MODELLING AND PID CONTROL SYSTEM OF FOUR ROTOR HELICOPTER
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
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