LINEAR ACTUATOR OF THRUST VECTORING CONTROL ON SOLID ROCKET MOTOR ON LAPAN SOUNDING ROCKET

Oka Sudiana, Khaula Nurul Hakim

Abstract


Rocket Technology Center of BRIN developed a rocket with a caliber of 450 mm with passive stability using four fins on tail. The next stage, Rocket Technology Center of BRIN designed a 450mm sounding rocket with canard fin control devices as active control on the rocket. In this paper, the thrust vector control (TVC) as an alternative control device is used. The TVC has been used since it has small thrust loss and large control torque. The linear actuator of the TVC on the Solid Rocket Motor (SRM) is studied. the linear actuator of the TVC is analyzed to understanding the behavior of the thrust vector control TVC movement during flight. The simulation shown that tunning the gain of the proportional-derivative controller generate variation the control of swing nozzle movement to get desire pitch angle. The result indicates the small control of TVC nozzle movement can produce pitch angle of rocket.

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References


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