• Title/Summary/Keyword: delay space

Search Result 637, Processing Time 0.029 seconds

THE HY-2 RADAR ALTIMETER AND SCATTEROMETER

  • Xu, Ke;Dong, Xiaolong;Zhang, Yunhua;Liu, Heguang
    • Proceedings of the KSRS Conference
    • /
    • v.1
    • /
    • pp.135-137
    • /
    • 2006
  • HY-2, the China's satellite for oceanic dynamic environment measurement, is planed to be launched around 2010. The main payloads of HY-2 include a dual-frequency radar altimeter equipped with a three-band nadir-looking radiometer for atmospheric delay correction, a Ku-band radar scatterometer, and a five-band scanning radiometer. This presentation outlines the specifications, parameters, and design of the HY-2 radar altimeter and scatterometer.

  • PDF

STABILITY LIMIT PROPERTIES OF CONTROL SYSTEMS ON THE SPACE OF ADJUSTING PARAMETERS (조정파라미터 공간에서의 제어계 안정한계 특성)

  • 최순만
    • Proceedings of the Korean Society of Marine Engineers Conference
    • /
    • 2000.11a
    • /
    • pp.135-142
    • /
    • 2000
  • The adjusting parameter set which enable control systems to locate on stability limit can be derived from theoretical or trial methods for an existing real system. The data from the results are much available to keep a system in the Proper stability condition even to site engineers who are inexperienced in the control system. In this paper, a general one loop control system was adopted for a model system the process of which was assumed to consist of a time-delay element and a first order-lag element in series. After obtaining the corresponding parameter set for the model system by mathematical procedures, their loci on the parameter space was taken according to frequency change. The parameter set loci of stability limit showed unique pattern, and particularity , the curves on the Kg-Ti parameter space were able to be generalized in the form of, an unique exponential formula. These properties were also compared with the results taken from experimental procedures by Nyquist response method and Ziegler & Nichols method on the time domain, and both results were confirmed to be nearly same.

  • PDF

A Study on the Interior Layout of the Rubber Wheel AGT lot the Passenger's comfortable circumstance (한국형 고무차륜AGT차량 승객의 안락한 공간 확보를 위한 최적 실내 공간 배치에 관한 디자인 연구)

  • 한석윤;최출헌;정종덕
    • Proceedings of the KSR Conference
    • /
    • 2000.05a
    • /
    • pp.463-470
    • /
    • 2000
  • The challenge to be faced in public transportation today is to satisfy human needs with the least delay, with the smallest number of accidents, and with the most economic use of energy, space, materials, man-power and money. One possible solution may lie in city train system, including AGT system. Specially, Passenger space in AGT is important to balance the budget of layout with passenger's satisfaction. This study focuses on lay-out and space, comfort which should be considered from the conceptual design stage of the interior layout work. Traditionally, the interior layout of the passenger room has emphasized ridequality and style. However, as the train becomes more prevalent and versatile, the focus also tends to shift toward layout and space to have comfortable circumstances. After all, the purpose of this research focused on arrangement a rational interior layout of the train through ergonomics research. Finally, the key was ensuring the comfortable environment based on cultural background of the passenger.

  • PDF

Accuracy Improvement of Multi-GNSS Kinematic PPP with EKF Smoother

  • Choi, Byung-Kyu;Sohn, Dong-Hyo;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
    • /
    • v.10 no.2
    • /
    • pp.83-89
    • /
    • 2021
  • The extended Kalman filter (EKF) is widely used for global navigation satellite system (GNSS) applications. It is difficult to obtain precise positions with an EKF one-way (forward or backward) filter. In this paper, we propose an EKF smoother to improve the positioning accuracy by integrating forward and backward filters. For the EKF smoother experiment, we performed PPP using GNSS data received at the DAEJ reference station for a month. The effectiveness of the proposed approach is validated with multi-GNSS kinematic PPP experiments. The EKF smoother showed 35%, 6%, and 22% improvement in east, north, and up directions, respectively. In addition, accurate tropospheric zenith total delay (ZTD) values were calculated by a smoother. Therefore, the results from EKF smoother demonstrate that better accuracy of position can be achieved.

Traffic Signal Control Algorithm for Isolated Intersections Based on Travel Time (독립교차로의 통행시간 기반 신호제어 알고리즘)

  • Jeong, Youngje;Park, Sang Sup;Kim, Youngchan
    • Journal of Korean Society of Transportation
    • /
    • v.30 no.6
    • /
    • pp.71-80
    • /
    • 2012
  • This research suggested a real-time traffic signal control algorithm using individual vehicle travel times on an isolated signal intersection. To collect IDs and passing times from individual vehicles, space-based surveillance systems such as DSRC were adopted. This research developed models to estimate arrival flow rates, delays, and the change rate in delay, by using individual vehicle's travel time data. This real-time signal control algorithm could determine optimal traffic signal timings that minimize intersection delay, based on a linear programming. A micro simulation analysis using CORSIM and RUN TIME EXTENSION verified saturated intersection conditions, and determined the optimal traffic signal timings that minimize intersection delay. In addition, the performance of algorithm varying according to market penetration was examined. In spite of limited results from a specific scenario, this algorithm turned out to be effective as long as the probe rate exceeds 40 percent. Recently, space-based traffic surveillance systems are being installed by various projects, such as Hi-pass, Advanced Transportation Management System (ATMS) and Urban Transportation Information System (UTIS) in Korea. This research has an important significance in that the propose algorithm is a new methodology that accepts the space-based traffic surveillance system in real-time signal operations.

A Comparison of Broadcast and Final Orbits on GPS Delays in GPS-VLBI Hybrid Observation

  • Kwak, Younghee;Cho, Jungho;Kondo, Tetsuro;Takiguchi, Hiroshi;Amagai, Jun;Gotoh, Tadahiro;Sekido, Mamoru;Ichikawa, Ryuichi;Kim, Tuhwan;Sasao, Tetsuo
    • Journal of Positioning, Navigation, and Timing
    • /
    • v.1 no.1
    • /
    • pp.65-75
    • /
    • 2012
  • We carry out an error analysis of 24-hour global positioning system (GPS)-very long baseline interferometry (VLBI) (GV) hybrid observation data. In this paper, we focus on the impacts of broadcast and final orbits on the GPS delays of the GV hybrid observation by analyzing the residuals, observed - calculated (O-C) values. The residuals show apparent and consistent biases for L1 and L2 signals, respectively. The scatters of the residuals are around a few nanoseconds. The main cause of those observation errors is the absence of the GPS phase and delay calibration system. Most of the satellites show that the differences between the delays, to which broadcast and final orbits are applied, are about 100 times smaller than the current GV hybrid observation errors. We conclude that GPS delays are not greatly affected by orbit accuracies.

Relationships between Diversity Techniques and Channel Coding Rates for OFDM and SC-FDE Systems (OFDM 및 SC-FDE 시스템에서의 다이버시티 기술과 채널부호화율의 상관관계)

  • Rim, Min-Joong
    • Journal of the Institute of Electronics Engineers of Korea TC
    • /
    • v.45 no.11
    • /
    • pp.23-31
    • /
    • 2008
  • This paper addresses relationships between diversity techniques and channel coding rates for OFDM and SC-FDE systems. In OFDM systems it is important to select proper channel coding rates according to multi-path channel profiles and low channel coding rates are required with cyclic delay diversity compared to the case of space time coding. On the other hand, it is not necessary to use low channel coding rates for SC-FDE systems where DFT spreading is applied to OFDM and relatively high channel coding rates can be used regardless of diversity techniques.

Human-in-the-Loop Simulation Analysis of Integrated RPAS Operations in Trajectory Based Operations Environment

  • Oh, Hyeju;Kang, Jisoo;Kang, Seon-Young;Choi, Keeyoung;Lee, Hak-Tae;Jung, Hyuntae;Moon, Woo-Choon
    • International Journal of Aeronautical and Space Sciences
    • /
    • v.17 no.4
    • /
    • pp.604-613
    • /
    • 2016
  • In this paper, Human-in-the-Loop (HiTL) simulations of Remotely Piloted Aircraft System (RPAS) operations in two different Air Traffic Management (ATM) concepts, conventional radar vectoring and Trajectory Based Operations (TBO), were performed to assess the impacts of RPAS integration in the future ATM environment. TBO concept maximizes the throughput by planning and sharing 4-D trajectories between pilots and controllers, and it is considered one of the key concepts to enable RPASs to operate with manned aircraft in congested airspaces. RPASs are characterized by having communication delay or temporary loss of communication. TBO capability was added to the integrated air traffic simulation system for this study, which was developed in the Inha University. HiTL simulations were performed by a trainee air traffic controller with three scenarios, and the data were analyzed using safety, efficiency, and controller workload metrics. The results suggest that TBO were effective in reducing delays and controller workload while maintaining the level of safety.

Fault Tolerant Attitude Control for a Spacecraft Using Reaction Wheels (반작용 휠을 사용하는 인공위성의 내고장 자세제어기법)

  • Jin, Jae-Hyun;Lee, Hun-Gu;Tahk, Min-Jea
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.35 no.6
    • /
    • pp.526-532
    • /
    • 2007
  • This paper considers a fault tolerant control problem for a spacecraft using reaction wheels. Faults are assumed to be inherent to only actuators(reaction wheels) and a control algorithm to accommodate actuators' faults is proposed. An attitude control loop includes an angular velocity control loop. The time delay control method is used to make a spacecraft follow the command angular velocity and to accommodate actuators' faults. A stability condition for the proposed algorithm is derived and the performance is demonstrated by computer simulations.

Unsteady Three-Dimensional Analysis of Transverse Fuel Injection into a Supersonic Crossflow using Detached Eddy Simulation Part II : Reacting Flowfield (DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 Part II : 반응 유동장)

  • Won, Su-Hee;Jeung, In-Seuck;Choi, Jeong-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.37 no.9
    • /
    • pp.879-888
    • /
    • 2009
  • Unsteady three-dimensional reacting flowfield generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using DES and finite-rate chemistry model. Comparisons are made with experimental results to investigate the turbulent reacting flow physics. The numerical OH distribution describes well the experimental OH-PLIF result, while the numerical ignition delay time shows some disparity due to the restricted available experimental data. The intermittency phenomena are identified by the comparative analysis between RANS and DES. Those effects are also quantified by the temperature distributions along streamlines and superimposed OH mass fraction along with time.