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 |