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Development of motion manipulator system for a generic aircraft flight dynamic simulator
Asalani Y.K.a, Sasongko R.A.a, Arifianto O.a
a Flight Physics Research Group, Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung, Bandung, 40132, Indonesia
[vc_row][vc_column][vc_row_inner][vc_column_inner][vc_separator css=”.vc_custom_1624529070653{padding-top: 30px !important;padding-bottom: 30px !important;}”][/vc_column_inner][/vc_row_inner][vc_row_inner layout=”boxed”][vc_column_inner width=”3/4″ css=”.vc_custom_1624695412187{border-right-width: 1px !important;border-right-color: #dddddd !important;border-right-style: solid !important;border-radius: 1px !important;}”][vc_empty_space][megatron_heading title=”Abstract” size=”size-sm” text_align=”text-left”][vc_column_text]© 2018 Authors.The purpose of this development program is to apply some prior studies about hexapod manipulator for designing aircraft simulator motion platform in terms of acceleration cue. Acceleration would represent human perception to describe a motion. By giving acceleration cues in a simulator, the operator would obtain similar sensation corresponding to real phenomenon/condition. Iteration process is used to collect relations between hexapod manipulator parameters, platform size and actuator position, and manipulator performances describing as manipulator displacement and acceleration range. Its kinematics and dynamics are modelled by using Newton-Euler approach and validated by using SimScape feature provided in MATLAB/Simulink. Hereafter, actuation control scheme would be implemented in order to convey manipulator from a conceptual world into real world based on its dynamics. As part of this development, constructing hexapod manipulator numerical model becomes the main objective of this current research.[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Author keywords” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Indexed keywords” size=”size-sm” text_align=”text-left”][vc_column_text]Acceleration cue,Aircraft simulator,Hexapod manipulator,Inverse dynamic,Newton-Euler approach,SimScape feature[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Funding details” size=”size-sm” text_align=”text-left”][vc_column_text]This work is part of research funded by the Ministry of Research and Higher Education (Kemenristekdikti) Republic of Indonesia.[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”DOI” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][/vc_column_inner][vc_column_inner width=”1/4″][vc_column_text]Widget Plumx[/vc_column_text][/vc_column_inner][/vc_row_inner][/vc_column][/vc_row][vc_row][vc_column][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][/vc_column][/vc_row]