2019
DOI: 10.1177/1077546319889786
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Simulation and adaptive control of back propagation neural network proportional–integral–derivative for special launcher using new version of transfer matrix method for multibody systems

Abstract: Rocket launcher system, as a special launcher placed on tactical vehicles, is a very complex mechanical system with characteristics of strong shock and vibration. In order to improve position accuracy, as well as reduce vibration, this paper creates a nonlinear dynamics model of the launcher system by using a new version of the transfer matrix method for multibody systems. The overall transfer equation of the nonlinear model is deduced. Combining with general kinematics equations of the rocket, the system laun… Show more

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Cited by 2 publications
(1 citation statement)
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“…To control the established underactuated dynamic system (Bessa et al, 2019), numerous studies with different methods have been successfully applied. These methods involve classical linear approaches such as proportional integral derivative (PID) control (Dong et al, 2017;Hoang et al, 2015;Miao et al, 2019), linear quadratic regulator control, and energy-based control (Cornejo and Alvarez-Icaza, 2011). Input shaping (Izadbakhsh and Kheirkhahan, 2018) has been widely used to eliminate system vibrations because of its simplicity and effectiveness.…”
Section: Introductionmentioning
confidence: 99%
“…To control the established underactuated dynamic system (Bessa et al, 2019), numerous studies with different methods have been successfully applied. These methods involve classical linear approaches such as proportional integral derivative (PID) control (Dong et al, 2017;Hoang et al, 2015;Miao et al, 2019), linear quadratic regulator control, and energy-based control (Cornejo and Alvarez-Icaza, 2011). Input shaping (Izadbakhsh and Kheirkhahan, 2018) has been widely used to eliminate system vibrations because of its simplicity and effectiveness.…”
Section: Introductionmentioning
confidence: 99%