Monte-Carlo Evaluation on Implementation of

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Monte-Carlo Evaluation on Implementation of

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dc.contributor.author Anukulsumpan, Nithi
dc.contributor.author Ratanaswasd, Palis
dc.contributor.author Khawsuk, Weerawat
dc.date.accessioned 2563-08-28T05:34:36Z
dc.date.available 2563-08-28T05:34:36Z
dc.date.issued 2559
dc.identifier.uri http://hdl.handle.net/123456789/2013
dc.description บทความวิจัย en_US
dc.description.abstract A simulation framework of a guided ballistic missile has been developed to aid the design and development of autopilot algorithm. In this framework, a hardware-in-the-loop (HIL) is utilized in the actuators that drive the control surfaces. The system dynamic engine is enhanced by receiving the position feedback of the actuator in real time allow it to be able to compute more realistic updates of system variables. A resistance torque emulator is introduced and deployed to further improve the realism of the dynamic engine. This allows the firmware control algorithm to better match the actual hardware in the real missile. An experiment is performed and results are used to compare with the simulation framework without HIL implementation. en_US
dc.description.sponsorship Defence Technology Institute en_US
dc.language.iso en en_US
dc.publisher Defence Technology Institute en_US
dc.relation.ispartofseries 5951;
dc.subject Simulation en_US
dc.subject Hardware-in-the-loop en_US
dc.subject Flight dynamics en_US
dc.subject Actuators en_US
dc.subject Canard en_US
dc.title Monte-Carlo Evaluation on Implementation of en_US
dc.type Article en_US


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