• Title/Summary/Keyword: All-Electric Aircraft power system

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A Voltage Bus Conditioner for a High Voltage DC Power Distribution System using High Performance Hysteresis Control (고성능 히스테리 제어를 이용한 고전압 DC 전력시스템을 위한 Voltage Bus Conditioner)

  • La, Jae-Du
    • The Transactions of the Korean Institute of Electrical Engineers P
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    • v.56 no.2
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    • pp.90-98
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    • 2007
  • More and All-Electric Aircraft (AEA) carry many loads with varied functions. In particular, there may be large pulsed loads with short duty ratio, which can affect the normal operation of other loads. In this paper, a bi-directional converter with inductive storage is used as a voltage bus conditioner (VBC) to mitigate voltage transients on the bus. In addition, the constant frequency hysteresis control technique for a VBC is presented. A simple and fast prediction of the hysteresis band-width is implemented by the phase-lock loop control, keeping constant switching frequency. This technique offers the excellent dynamic response in load or parameter variation. The control performance is illustrated by simulated results with the SABER package, The proposed hysteresis control results in the shortest and the smallest excursions.

The State of the Art and Application of Actuator in Aerospace (항공우주용 구동장치 개발 동향)

  • Yoon, Gi-Jun;Park, Ho-Youl;Jang, Ki-Won
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.6
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    • pp.89-102
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    • 2010
  • In this paper, a study on the future-oriented actuator introduces the future technology and future direction in aerospace and several industry fields. In particular, the mechanical linkage or hydraulic and pneumatic actuators which have the higher output-to-weight ratio have been used a lot in the past as the aircraft's flight control device. Most recently, Fly-By-Wire system has been used in aircraft and the flight control system has been changed in more electric and all electric systems. Electrohydraulic actuators and electric actuators have been developed continually, because they have better efficiency, safety and lower cost for the flight control system of aircraft. Also, to improve the weight condition, accuracy and response of actuator, new field actuators using new materials have been developed. In this paper we clearly proposed the actuator design and detailed technology development trend for next generation actuation system in aerospace and new field.

Analysis of Development Trend for the Integrated Power System of Naval Vessels to Perform the High-Power and Energy Mission Load Platform (고출력 에너지 사용 체계 플랫폼 실현을 위한 해군함정의 통합 동력 시스템 발전 경향 분석)

  • Lee, Hyung-Min;Cho, Byung-Jin
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.6
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    • pp.796-801
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    • 2011
  • The objective of this work presented here was focused on analysis of development trend for the integrated power system of naval vessels to perform the high-power and energy mission load platform. These mission loads are affected by the high level of military technologies, digitalization of the ocean battlefield, high power sensor system for maximization of the ship survivability. All electric power including propulsion power for ship should be controlled by integrated single system in order to carry various high power density weapon system such as Electromagnetic Aircraft Launch System, Electromagnetic Rail Gun[feasible precision striking at long distance 200NM(370km) or over]. As the analyzing the present state of things, mechanical propulsion system is shifted into hybrid or fully electric propulsion systems to realize integrated power system at the developed countries. Such challenges include reduced dependency on foreign-supplied fossil fuel, increasing demand for installed ship power, controlling life-cycle costs.

The Comparison of Two Control Algorithm for a Voltage Bus Conditioner in a DC Power Distribution System (DC 전력시스템에서의 Voltage Bus Conditioner의 제어기법 비교)

  • La, Jae-Du;Lee, Yong-Geun
    • The Transactions of the Korean Institute of Electrical Engineers P
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    • v.55 no.1
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    • pp.47-53
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    • 2006
  • A Voltage Bus Conditioner (VBC) is used to mitigate the voltage transients on a common power distribution bus. The VBC described here utilises inductive storage and unlike its counter part with capacitive storage, it can employ the entire stored energy towards transients' mitigation. The performances of adaptive duty ratio control and sliding mode control have been compared. The simulation results (with the package SABER) indicate that the sliding mode control results in the shortest and the smallest bus voltage excursions.

An Improved Adaptive Control Technique for the Voltage Bus Conditioner with the Reduced Capacitive Storage (축소된 캐패시터 스토리지를 갖는 Voltage Bus Conditioner의 향상된 적응제어)

  • La, Jae-Du;Lee, Yong-Geun
    • The Transactions of the Korean Institute of Electrical Engineers P
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    • v.60 no.1
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    • pp.13-18
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    • 2011
  • More and all-electric aircraft (AEA) carry many loads with varied functions. In particular, there may be large pulsed loads with short duty ratios which can affect the normal operation of other loads. In this paper, a converter with spilt capacitors and an improved adaptive controller is used as the Voltage Bus Conditioner (VBC) with the reduced capacitive storage to mitigate the voltage transients on the bus. The proposed converter allows the smaller capacitive storage. Also, the proposed controller has the advantage of requiring only one sensor and performing both the functions of mitigating the voltage bus transients and maintaining the level of energy stored. Experimental results are presented which verify the control principles and demonstrate the practicality of the approach.