• 제목/요약/키워드: Absolute Altitude

검색결과 34건 처리시간 0.024초

기준국을 이용한 실내·외 절대 고도 산출 및 3D 항법 (Absolute Altitude Determination for 3-D Indoor and Outdoor Positioning Using Reference Station)

  • 최종준;최현영;도승복;김현수
    • 한국통신학회논문지
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    • 제40권1호
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    • pp.165-170
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    • 2015
  • 본 논문은 3D 위치 정보를 산출하기 위한 기압고도계 및 기준국을 이용한 절대 고도 측정 정확도 향상에 관한 연구이다. GPS와 같은 위성 항법 시스템이 신뢰성이 있는 절대 고도를 제공하지 못하는 점과 기압 고도계가 변화하는 대기압의 특성상 절대 고도 정보를 제공하지 못한다는 문제점을 인식하고, 이를 개선하기 위해 새로운 기법을 제안하였다. 제안된 기법을 검증하기 위해 RTK를 활용한 기준국을 지정하고 시중에 판매하는 압력 센서 및 EVK 단말기를 활용하였으며, 실내 외에서의 사람의 이동으로 인한 고도 변화 실험과 차량을 이용한 이동 실험을 통해 검증하였다. 이 논문의 결과는 기준국을 이용하는 기존의 2D 측위 시스템을 간단히 3D 측위 시스템으로 확장할 수 있는 저가 솔루션을 제공할 수 있음을 보였다.

실용상승한도 고도 부근에서 무인기의 속도 및 고도유지 제어에 관한 연구 (Study on Velocity and Altitude Keeping Method of a UAV Around Service Ceiling Altitude)

  • 홍진성;원대연;장세아
    • 한국항공우주학회지
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    • 제49권5호
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    • pp.383-388
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    • 2021
  • 항공기에 사용되는 공기 흡입식 엔진은 고도가 높아질수록 성능의 한계를 가지며, 이는 실용상승한도(Service Ceiling)와 절대상승한도(Absolute Ceiling) 고도로 나타나게 된다. 고정익 항공기가 순항비행(Level Flight) 상태에서 고전제어기법(Classical Control)을 사용하여 고도 및 속도 유지를 하는 방법은 일반적으로 속도 증/감속을 위해 추력을 사용하고, 고도 증/감을 위해 피치 자세를 사용한다. 실용 상승 한도 고도 부근에서 이 방법을 사용하는 경우 고도 오차를 줄이기 위해 피치를 증가시키면 속도 감속으로 나타나게 된다. 따라서 피치 자세를 사용하여 속도를 먼저 유지하는 방법을 사용해야 한다. 특히 무인기의 경우 이 두 가지의 방법을 자동으로 적절한 시점에 사용할 수 있어야 한다. 본 논문에서는 고도 상승률이 둔화되는 실용상승한도 부근에서 속도와 고도유지 알고리즘의 전환 방법을 제안하고, 비행시험을 통해 개선된 효과를 확인하였다.

기압 고도계를 이용한 DGPS 고도측정 향상 (Altitude Estimation Improvement in DGPS using Barometric Altitude Sensors)

  • 유호;이영재;지규인;천세범;권철범;전향식;주정민
    • 한국항공우주학회지
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    • 제34권1호
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    • pp.89-94
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    • 2006
  • DGPS는 GPS위성배열의 기하학적인 특성에 따라 수평면 정확도에 비해 고도 정확도가 좋지 않다. DGPS고도를 보정하기위해 두 개의 기압고도계를 사용하였고 각각 이동국과 기준국에 설치하여 차분된 고도를 얻어냈다. 이 차분된 고도는 DGPS 고도측정치와 칼만필터로 결합하여 향상된 고도를 추정한다. 이와 같은 차분된 고도는 기존의 상대고도에 기반을 두고 있지만 압력 고도가 아닌 절대고도를 주는 것에 차이가 있다. 또한 기저선의 변화에 따라 차분된 고도가 얼마나 정확성을 갖고 있는지 실제 실험을 통해 확인한다.

서해안 인접공항의 저고도 항공기상 정확도 연구 (A Study on Accuracy of Meteorological Information for Low Altitude Aerospace around the Airport on the West Coast)

  • 조영진;유광의
    • 한국항공운항학회지
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    • 제28권2호
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    • pp.53-62
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    • 2020
  • This study is to evaluate the accuracy of the meteorological information provided for the aircraft operating at low altitude. At first, it is necessary to identify crucial elements of weather information closely related to flight safety during low altitude flights. The study conducted a survey of pilots of low altitude aircraft, divided into pre-flight and in-flight phases, and reached an opinion that wind direction, wind speed, cloud coverage and ceiling and visibility are important items. Related to these items, we compared and calculated the accuracy of TAFs and METARs from Taean Airfield, Seosan Airport and Gunsan Airport because of their high number of domestic low-altitude flights. Accuracy analysis evaluated the accuracy of two numerical variables, Mean Absolute Error(MAE) and Root Mean Square Error(RMSE), and the cloud coverage which is categorical variable was calculated and compared by accuracy. For numeric variables, one-way ANOVA, which is a parameter-test, was approached to identify differences between actual forecast values and observations based on absolute errors for each item derived from the results of MAE and RMSE accuracy analyses. To determine the satisfaction of both normality assumptions and equivalence variability assumptions, the Shapiro-Wilk test was performed to verify that they do not have a normality distribution for numerical variables, and for the non-parametric test, Kruscal-Wallis test was conducted to determine whether or not they are satisfied.

A Study on Altitude Estimation using Smartphone Pressure Sensor for Emergency Positioning

  • Shin, Donghyun;Lee, Jung Ho;Shin, Beomju;Yu, Changsu;Kyung, Hankyeol;Choi, Dongwook;Kim, Yeji;Lee, Taikjin
    • Journal of Positioning, Navigation, and Timing
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    • 제9권3호
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    • pp.175-182
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    • 2020
  • This paper introduces a study to estimate the user altitude in need of rescue in an emergency. The altitude is estimated by using the barometric pressure sensor embedded in the smartphone. Compared to GPS, which is degraded in urban or indoor environments, it has the advantage of not having spatial restrictions. With the endless development of smartphone hardware, it is possible to estimate the absolute altitude using the measured value if only the bias of the embedded barometric pressure sensor is applied. The altitude information of the person in need of rescue in an emergency is a great help in reducing rescue time. Since time is tight, we propose online calibration that provides the barometric pressure sensor bias used for altitude estimation through database. Furthermore, experiments were conducted to understand the characteristics of the barometric pressure sensor, which is greatly affected by wind. At the end, the altitude estimation performance was confirmed through an actual field tests in various floors in the building.

대기압이 가스유량측정에 미치는 영향에 관한 연구 (A Study on the Effect of the Atmospheric Pressure in the Gas Flow Measurement)

  • 정종태;하영철;이철구;허재영
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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    • pp.363-369
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    • 2002
  • Orifice meter is the most widely used flowmeter in custody transfer between KOGAS and city gas companies. Absolute pressure value is needed to calculate the gas flow of orifice metering system, but the gauge pressure transmitters are mainly used in the field. In case that the gauge pressure transmitters are used, the fixed value as standard atmospheric pressure(101.325kPa) is applied for the absolute pressure value. The real, local atmospheric pressures of each metering station are different from the standard condition as the altitude and weather conditions. In this study the flow calculation errors were quantitatively analyzed through examining the atmospheric pressures of 50 stations of KOGAS. The data for analysis are such like the time data of supplied gas amount, the altitude of each metering station, the time data of atmospheric pressures and altitudes of each weather observatory. The results showed that the local atmospheric pressures were different from the standard value and the gas flow calculation errors were distributed between $-0.024\%{\~}0.025\%$ based on the supplied gas amount in the year 1999 and 2000.

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농업기상 결측치 보정을 위한 통계적 시공간모형 (A Missing Value Replacement Method for Agricultural Meteorological Data Using Bayesian Spatio-Temporal Model)

  • 박다인;윤상후
    • 한국환경과학회지
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    • 제27권7호
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    • pp.499-507
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    • 2018
  • Agricultural meteorological information is an important resource that affects farmers' income, food security, and agricultural conditions. Thus, such data are used in various fields that are responsible for planning, enforcing, and evaluating agricultural policies. The meteorological information obtained from automatic weather observation systems operated by rural development agencies contains missing values owing to temporary mechanical or communication deficiencies. It is known that missing values lead to reduction in the reliability and validity of the model. In this study, the hierarchical Bayesian spatio-temporal model suggests replacements for missing values because the meteorological information includes spatio-temporal correlation. The prior distribution is very important in the Bayesian approach. However, we found a problem where the spatial decay parameter was not converged through the trace plot. A suitable spatial decay parameter, estimated on the bias of root-mean-square error (RMSE), which was determined to be the difference between the predicted and observed values. The latitude, longitude, and altitude were considered as covariates. The estimated spatial decay parameters were 0.041 and 0.039, for the spatio-temporal model with latitude and longitude and for latitude, longitude, and altitude, respectively. The posterior distributions were stable after the spatial decay parameter was fixed. root mean square error (RMSE), mean absolute error (MAE), mean absolute percentage error (MAPE), and bias were calculated for model validation. Finally, the missing values were generated using the independent Gaussian process model.

MEMS INS 기반 건설현장작업자의 3D 위치결정기법에 관한 연구 (Research of MEMS INS Based 3D Positioning Technologies for Workers in Construction Field)

  • 장용구;김현수;도승복;전흥수
    • 한국지반환경공학회 논문집
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    • 제14권3호
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    • pp.51-60
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    • 2013
  • 본 연구에서는 기압 센서의 특성과 기존의 차분 기법을 결합하여 임의의 건설현장에서 작업자의 절대고도를 확보하는 방법을 제안하고, 다양한 특성을 가진 다양한 건설 현장에서 이 방법을 적용한 결과를 분석하여 그 타당성을 검증하였다. 본 연구 결과물은 실제 건설 현장에서 작업자의 3D좌표 추출에 적용하기 위한 실용 기술로 개발된 것으로써 스마트폰에 내장된 각종 MEMS 센서들의 사양과 특징을 분석하고 데이터를 획득하여 단말기의 위치를 실내외에서 어떻게 결정할 수 있는지를 각종 시험을 통해 검증하였다. 이를 위해 다양한 실제 스마트폰으로부터 센서정보를 추출하는 프로그램을 개발하고 PC인터페이스 방법을 제시하였으며 개발과정에서 발생한 여러 문제점들을 극복하는 방안 등을 소개한다.

심해저 망간단괴 집광기의 채집장치에 관한 연구 (A Study on Pick-up Device of Beep Sea Manganese Nodules Collector)

  • 홍섭;심재용;이태희;최종수
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1996년도 추계학술대회 논문집
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    • pp.891-895
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    • 1996
  • Performance and efficiency of hybrid (hydraulic-mechanical) pick-up device of deep sea manganese nodules collector are very sensitive to altitude and altitude of pick-up head relative to undulating seafloor. For this reason, motion control of pick-up head relative to the changing deep sea topography and other disturbances is of particular importance in design of pick-up device. The concept of design axiom is applied to a pick-up device of hybrid type. Kinematic analysis conducted in absolute Cartesian coordinates gives position, velocity, and acceleration of the hydraulic cylinders which enable the pick-up head to keep the preset optimal distance from seafloor. Inverse dynamic analysis provides the driving forces of hydraulic cylinders and the reaction forces at each joint. Design sensitivity analysis is performed in order to investigate the effects of possible design variables on the change of the maximum strokes of hydraulic cylinders. The direct differentiation method is used to obtain the design sensitivity coefficients.

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Performance Improvement of an INS by using a Magnetometer with Pedestrian Dynamic Constraints

  • Woyano, Feyissa;Park, Aangjoon;Lee, Soyeon
    • IEIE Transactions on Smart Processing and Computing
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    • 제6권1호
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    • pp.1-9
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    • 2017
  • This paper proposes to improve the performance of a strap down inertial navigation system using a foot-mounted low-cost inertial measurement unit/magnetometer by configuring an attitude and heading reference system. To track position accurately and for attitude estimations, considering different dynamic constraints, magnetic measurement and a zero velocity update technique is used. A conventional strap down method based on integrating angular rate to determine attitude will inevitably induce long-term drift, while magnetometers are subject to short-term orientation errors. To eliminate this accumulative error, and thus, use the navigation system for a long-duration mission, a hybrid configuration by integrating a miniature micro electromechanical system (MEMS)-based attitude and heading detector with the conventional navigation system is proposed in this paper. The attitude and heading detector is composed of three-axis MEMS accelerometers and three-axis MEMS magnetometers. With an absolute algorithm based on gravity and Earth's magnetic field, rather than an integral algorithm, the attitude detector can obtain an absolute attitude and heading estimation without drift errors, so it can be used to adjust the attitude and orientation of the strap down system. Finally, we verify (by both formula analysis and from test results) that the accumulative errors are effectively eliminated via this hybrid scheme.