• 대한전자공학회:학술대회논문집
• /
• 대한전자공학회 2002년도 하계종합학술대회 논문집(1)
• /
• pp.291-294
• /
• 2002

This paper proposed interface test method for performance verification of communication and broadcasting satellite between communication and broadcasting satellite payload and EGSE(Electrical Ground Support Equipment). We need ground support equipment for test them to performance verification and conform interface function of payload. This paper define tile telemetry transfer method for control payload using GSE(Ground Support Equipment) and receive telemetry data collected from GSE through bus simulator

• 한국자동차공학회논문집
• /
• 제19권2호
• /
• pp.133-141
• /
• 2011

The effect of payload on fuel consumption and emission of light duty freight truck during acceleration driving has been analyzed. Running tests were carried out with various payload conditions on chassis dynamometer. A typical driving pattern for urban cities was used. Real time emission measurement systems for gaseous and soot emission were utilized to investigate the real time dynamic of fuel use and exhaust emissions. It was observed that fuel use and pollutant emissions were increased as payload was increased. Under the same payload condition, the increased amount of acceleration driving is much higher than that of steady state driving. The results demonstrated the advantages of eco-driving, which is an environmentally friendly driving manner, could be emphasized in heavier payload condition. Inertial tractive power was introduced for considering the parameters affecting emission during acceleration driving, which are speed, acceleration and payload. Fuel use and emission in various driving conditions were expressed as functions of inertial tractive power. The estimated result by these functions well predicted measured result within 10 % deviation.

• 항공우주시스템공학회지
• /
• 제11권2호
• /
• pp.30-34
• /
• 2017

본 고찰은 위성시스템을 구성하는 본체, 고해상도 카메라로 대표되는 주탑재체 및 과학임무용으로 사용되는 과학 목적 및 기술검증용 탑재체 중 본체와 주탑재체를 제외한 탑재체에 대한 제품보증 방안에 관한 것이다. 현재까지 우리나라는 위성 개발 프로그램을 통해 위성 본체 및 주탑재체에 대한 제품보증을 성공적으로 수행하여 왔다고 할 수 있다. 다만, 모든 위성 개발 프로그램에서 개발예산과 기간에 제한이 있음을 고려할 때, 본체나 주탑재체와 비교시 그 중요도가 상대적으로 낮다고 할 수 있는 과학 및 기술검증용 탑재체에 대한 적정한 제품보증 수준을 결정하는 것은 매우 중요하다. 본 고찰은 이러한 관점에서 과학 및 기술검증용 탑재체에 대한 제품보증 방향을 모색하기 위한 것이다.

• Journal of Astronomy and Space Sciences
• /
• 제13권2호
• /
• pp.117-133
• /
• 1996

In this paper, we describe the architecture and protoccl of stored-and-forward packet communication payload of KITSAT 1/2 microsatellites and then analyze this payload in terms of the probabilities of login success and login refusal, and maximum throughput as quality of service parmaeters.

• 한국소음진동공학회논문집
• /
• 제21권12호
• /
• pp.1146-1151
• /
• 2011

Acoustic load from rocket propulsion system is main source of random vibration working on the payload. To protect payload from this acoustic load, additional APS(acoustic protection system) is generally applied. Noise reduction capacity of APS can be verified through acoustic test and vibro-acoustic coupled analysis. This paper compared the results of acoustic test and vibro-acoustic coupled analysis about KSLV-I payload fairing with APS.

• International Journal of Control, Automation, and Systems
• /
• 제1권1호
• /
• pp.43-53
• /
• 2003

A modified command shaping control to reduce residual vibrations at a target position and to limit the sway angle of the payload during traveling for container crane systems is investigated. When the maneuvering time is minimized, a large transient amplitude and steady state oscillations may occur inherently. Since a large swing of the payload during the transfer is dangerous, the control objective is to transfer a payload to the desired place as quickly as possible while limiting the swing angle of the payload during the transfer. The conventional shapers have been enhanced by adding one more constraint to limit intermediate sway angles of the payload. The developed method is shown to be more effective than other conventional shapers for prevention of an excessive transient sway. Computer simulation results are provided.

• 대한원격탐사학회:학술대회논문집
• /
• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
• /
• pp.225-228
• /
• 2005

Telescope structure based on Korsch type optical layout was suggested for a large aperture optical system. Korsch type optical layout is regarded as providing wide field of view and no color aberration for which high resolution space cameras greatly demand. For the suggested Korsch type telescope structure, two folding mirrors are adopted, firstly to provide for the refocusing device mounting plane on the second fold mirror assembly, secondly by double folding the light path to concisely confine focal plane assembly within the perimeter of the tube. Optical layput design and corresponding support structure design were attained.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2008년도 학술대회 논문집 정보 및 제어부문
• /
• pp.369-370
• /
• 2008

The Payload Interface Unit (PIU) provides the interface between payload equipment (GOCI, MODCS and Ka Band P/L) and the SCU. The PIU is a MIL-STD-1553-Bus Remote Terminal (RT). The MPIU distributes commands to, acquires telemetry from and takes part in the thermal control of the payload equipment. When in ON mode, the PIU is completely observable and can be used for payload control. When in OFF mode, the PIU is non active except the thermal control electronics.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2007년도 춘계학술대회논문집
• /
• pp.220-223
• /
• 2007

Acoustic test of the payload fairing of Korea satellite launch vehicle was conducted to verify the performance of acoustic protection system installed inside the payload fairing. This paper briefly introduces the acoustic test procedures and its results. Overall 148 dB acoustic loads were exerted on the payload fairing structures which mated with the upper stage structure of the launch vehicle. In order to verify the increase of insertion loss by the acoustic protection system, two kinds of test were performed. One is conducted with acoustic protection system and the other without acoustic protection system. Internal acoustic loads as well as external ones were measured and the measured insertion losses were compared with the requirement. The results showed that the acoustic protection system increases the insertion loss by more than 6 dB above 125 Hz. They also indicated that some design modification of Helmholtz resonator array is required to increase the insertion loss at a cavity resonant frequency.

• Journal of Astronomy and Space Sciences
• /
• 제15권2호
• /
• pp.509-523
• /
• 1998

군 통신위성 탑재 체의 개념모델(payload Concept Model; PCM) 연구는 실제 위성의 설계 및 제작 이전에 탑재 체를 지상에서 상용부품으로 구성하고 실제 위성과 가까운 통신전파 조건에서 시험하여 그 특성과 성능을 미리 파악하고자 하는 것이다. 본 논문에서는 이러한 통신 탑재 체 개념 모델을 구현하기 위한 기계구조물의 설계와 제작 과정을 기술하고 있다. 제작된 개념모델의 설계 조건의 만족여부를 검증하기 위하여 기본 RF 특성 시험을 실시하였으며 시스템이 양호한 통신품질을 제공함과 정상적으로 작동됨이 확인되었다.