Abstract:
일 실시 예에 따르면, 무인 비행체에 탑재 가능한 시료 처리 장치는, 공기 중의 시료를 수용 가능한 챔버; 상기 시료의 유동 방향을 기준으로, 상기 챔버의 상류 측에 형성되고, 상기 시료를 상기 챔버 내로 안내하기 위한 이송부; 및 상기 시료의 유동 방향을 기준으로, 상기 챔버의 하류 측에 장착되어 상기 시료의 유동 방향을 형성하기 위한 팬을 포함하고, 상기 이송부는 상기 챔버와 연통되는 이송관; 및 이송관 상에 형성된 유입구를 포함할 수 있다.
Abstract:
본 발명은 DutyCycle기반의 MAC 프로토콜에서 채널 환경에 따라 Wakeup period(구간 또는 기간)를 동적으로 가변화시키는 방법에 관한 것으로, DutyCycle의 Wakeup 구간에서 체크한 채널 상태를 근거로 이웃 노드의 트래픽을 카운트하여, 상기 카운트된 이웃노드의 트래픽에 따라 동일 Duty Cycle내에서의 Wakeup 구간을 동적으로 가변시킴으로써 수신 성공률 및 에너지 효율을 향상시킬 수 있다.
Abstract:
A target following clustering algorithm of the present invention generates or eliminates a cluster dependently following a target when detecting the target in surveillance reconnaissance applications, thereby sensitively responding to motions of the target even when traffic of a wireless sensor network bursts locally by the detected target. Also, it is possible to improve energy efficiency since both a boundary problem and a blackhole can be resolved. Moreover, the target following clustering algorithm reduces costs of system maintenance in the military with weak electricity infrastructures and has high applicability by reducing energy consumption in the wireless sensor network and prolonging the lifetime, namely, duration time of the network.
Abstract:
The present invention relates to a method for dynamically varying a wakeup period (interval or period) according to channel environments in a duty cycle-based MAC protocol, which is capable of improving a reception success rate and energy efficiency by counting the traffic of a neighboring node based on a channel state checked in the wakeup period within the duty cycle, and dynamically varying the wakeup period within the same duty cycle according to the counted traffic of the neighboring node.
Abstract:
PURPOSE: A position control system and method for a driving device of a counter-shell launcher for active defense are provided to ensure improved control performance by removing the influences by modeling errors, disturbance, and measurement noises. CONSTITUTION: A position control system for a driving device of a counter-shell launcher for active defense comprises a reference position information input unit(110), a drive unit(130), a numerical differentiator(140), a kalman filter, and a controller(120). The reference position information input unit provides reference position information for position control of the drive unit. The drive unit has a driver(132) and a motor(135). The numerical differentiator calculates the speed of the drive unit by differentiating the position of the drive unit measured by a resolver(136) of the motor. The kalman filter calculates the estimated speed value of the drive unit from the speed of the drive unit calculated by the numerical differentiator and the position of the drive unit measured by the resolver. The controller controls the position of the drive unit to using position control algorithm based on the reference position, position errors, and the estimated speed value.