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      항공무장 안정성 향상을 위한 날개 전개 구동기의 작동로직 설계 = Deployment Actuator Logic Design for Enhancing Aircraft Armament Stability

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      https://www.riss.kr/link?id=A109023447

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      For the high reliability of guidance weapon, it is important to maintain the stable supply voltage for guidancesystem while the bomb is gliding. However, the DC motor drive for guidance control in the low temperature canlead to the critical voltage drop due to a large inrush current.
      In this paper, we propose the wing deployment logic design to enhance the guidance system stability. To derivethe stable drive logic based on PWM, we controlled the duty cycles for input voltage of DC motor in lowtemperature. The initial duty cycle was set to 40 % to relieve the inrush current. Moreover, the proper time,which is less than 1 second for controlling duty cycles, was determined by the iterative wing deployments ofguidance kit. Finally, the validity of proposed logic was confirmed from the result the maximum voltage drop forthe wing deployment was decreased by 23 %.
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      For the high reliability of guidance weapon, it is important to maintain the stable supply voltage for guidancesystem while the bomb is gliding. However, the DC motor drive for guidance control in the low temperature canlead to the critical voltage dr...

      For the high reliability of guidance weapon, it is important to maintain the stable supply voltage for guidancesystem while the bomb is gliding. However, the DC motor drive for guidance control in the low temperature canlead to the critical voltage drop due to a large inrush current.
      In this paper, we propose the wing deployment logic design to enhance the guidance system stability. To derivethe stable drive logic based on PWM, we controlled the duty cycles for input voltage of DC motor in lowtemperature. The initial duty cycle was set to 40 % to relieve the inrush current. Moreover, the proper time,which is less than 1 second for controlling duty cycles, was determined by the iterative wing deployments ofguidance kit. Finally, the validity of proposed logic was confirmed from the result the maximum voltage drop forthe wing deployment was decreased by 23 %.

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      참고문헌 (Reference)

      1 S. -T. Jung, "Voltage Restorers of PM Synchronous Generator" 512-513, 2013

      2 배종진 ; 최성재 ; 정호락 ; 박문수 ; 박현종, "Transfer Function Model Development of Fuel-draulic Actuator for Launch Vehicle and Parameter Estimation Using Genetic Algorithm" 51 (51): 415-422, 2023

      3 윤기준 ; 박호열 ; 장기원, "The State of the Art and Application of Actuator in Aerospace" 14 (14): 89-102, 2010

      4 H. A. Gabbar, "Review of Battery Management Systems(BMS)Development and Industrial Standards" 9 (9): 1-23, 2021

      5 J. Y. Lee, "Indirect Measurement of Torque of the Auto Screw Drive to Using the Current Signals of DC Motor" 299-304, 2003

      6 "Global Climatic Data for Developing Military Products" Department of Defence(DoD)

      7 K. Chen, "Evaluation of the low temperature performance of lithium manganese oxide/lithium tianate lithium-ion batteries for start/stop applications" 278 : 411-419, 2015

      8 K. Lee, "Design of the Medium-Range GPS Guided Kit" 584-587, 2013

      9 S. Lee, "Analysis of Driving Characteristics on Airborne Equipment" 1014-1015, 2018

      10 이호성, "A Study on the Torque Control Method of a Hydraulic Actuation System for Measuring the Dynamic Stiffness of Missle Fin Actuators" 10 (10): 181-188, 2007

      1 S. -T. Jung, "Voltage Restorers of PM Synchronous Generator" 512-513, 2013

      2 배종진 ; 최성재 ; 정호락 ; 박문수 ; 박현종, "Transfer Function Model Development of Fuel-draulic Actuator for Launch Vehicle and Parameter Estimation Using Genetic Algorithm" 51 (51): 415-422, 2023

      3 윤기준 ; 박호열 ; 장기원, "The State of the Art and Application of Actuator in Aerospace" 14 (14): 89-102, 2010

      4 H. A. Gabbar, "Review of Battery Management Systems(BMS)Development and Industrial Standards" 9 (9): 1-23, 2021

      5 J. Y. Lee, "Indirect Measurement of Torque of the Auto Screw Drive to Using the Current Signals of DC Motor" 299-304, 2003

      6 "Global Climatic Data for Developing Military Products" Department of Defence(DoD)

      7 K. Chen, "Evaluation of the low temperature performance of lithium manganese oxide/lithium tianate lithium-ion batteries for start/stop applications" 278 : 411-419, 2015

      8 K. Lee, "Design of the Medium-Range GPS Guided Kit" 584-587, 2013

      9 S. Lee, "Analysis of Driving Characteristics on Airborne Equipment" 1014-1015, 2018

      10 이호성, "A Study on the Torque Control Method of a Hydraulic Actuation System for Measuring the Dynamic Stiffness of Missle Fin Actuators" 10 (10): 181-188, 2007

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