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Dynamic Response Simulation and Analysis of Highly Maneuverable Aircraft in the Presence of Control Devices Failures
Arif A.A.a, Wandini R.A.a, Sasongko R.A.a
a Institut Teknologi Bandung, Faculty of Mechanical and Aerospace Engineering, 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]© 2019 IEEE.A highly maneuverable aircraft, such as fighter aircraft, relies significantly on the performance of its control devices for executing aggressive and non-conventional maneuvers, and also for executing other routine tasks. Any defect or failure that may happen on the control device actuators can reduce the controllability of the aircraft, even can bring it to a catastrophic condition. A study on the effect of defected/failure control device has on the aircraft closed-loop response during some predefined maneuvers is described in this paper. It is intended to identify and analyze the aircraft dynamic behavior when one of its control surfaces is failed in particular flight phases. The failure is modeled as changes in the dynamic characteristics of the actuator, which is affected by the load generated on the control surface during maneuvers. The change of the actuator behavior affects the performance of the closed- loop system and may result in excessive control command/deflection in order to maintain control authority. The proposed approach may be exploited to examine the effect of control device failures has on the performance of fighter aircraft in executing a mission.[/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]Aircraft dynamics,Closed loop response,Control authorities,Control command,Control device,Dynamic characteristics,Dynamic response simulation,Flight phasis[/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]Control surface failure,Flight Control,Flight Dynamics,Stability[/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][/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]https://doi.org/10.1109/ACDT47198.2019.9072873[/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]