• 제목/요약/키워드: Baseline Length Constraint

검색결과 8건 처리시간 0.027초

Performance Improvement of Wald Test for Resolving GPS Integer Ambiguity Using a Baseline-Length Constraint

  • Lee Eun-Sung;Chun Se-Bum;Lee Young-Jae;Kang Tea-Sam;Jee Gyu-In;Abdel-Hafez Mamoun F.
    • International Journal of Control, Automation, and Systems
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    • 제4권3호
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    • pp.333-343
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    • 2006
  • In this paper, the baseline-length information is directly modeled as a measurement for the Wald test, which speeds up the resolution convergence of the integer ambiguity of GPS carrier phase measurements. The convergent speed improvement is demonstrated using numerical simulation and real experiments. It is also shown that the integer ambiguities can be resolved using only four actual satellite measurements with very reasonable convergence speed, if the baseline-length information is used just like one additional observable satellite measurement. Finally, it is shown that the improvement of convergence speed of the Wald test is due to the increase of the probability ratio with the use of the baseline-length constraint.

Kinematic GPS Positioning with Baseline Length Constraint Using the Maximum Possibility Estimation Method

  • Wang, Xinzhou;Xu, Chengquan
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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    • pp.247-250
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    • 2006
  • Based on the possibility theory and the fuzzy set, the Maximum Possibility Estimation method and its applications in kinematic GPS positioning are presented in this paper. Firstly, the principle and the optimal criterion of the Maximum Possibility Estimation method are explained. Secondly, the kinematic GPS positioning model of single epoch single frequency with baseline length constraint is developed. Then, the authors introduce the artificial immune algorithm and use this algorithm to search the global optimum of the Maximum Possibility Estimation model. The results of some examples show that the method is efficient for kinematic GPS positioning.

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GPS를 이용한 자세 측정 시스템의 미지정수 결정기법 (An Integer Ambiguity Resolution Method for GPS Attitude Determination)

  • 박찬식;김일선
    • 제어로봇시스템학회논문지
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    • 제5권1호
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    • pp.62-68
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    • 1999
  • The attitude of a vehicle can be precisely determined using GPS carrier phase measurements from more than two antennas attached to a vehicle and an efficient integer ambiguity resolution technique. Many methods utilizing the known baseline length as a constraint of independent elements of integer ambiguities are proposed to resolve integer ambiguity at real time. Three-dimensional search space is reduced to two-dimensional search space with this constraint. Thus the true integer ambiguity can be easily determined with less computational burden and fewer number of measurements. But there are still strong requirements for the real time integer ambiguity resolution, which uses single epoch measurement of long baseline. In this paper, a new constraint from the geometry of multiple baselines is derived. With this new constraint, two-dimensional search space is further reduced to one-dimensional search space. It makes possible to determine integer ambiguity with single epoch measurement. The proposed method is applied to real data to show its effectiveness.

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An efficient Ambiguity searching method with constraints for attitude finding GPS receivers

  • Nam, Sung-Il;Son, Seok-Bo;Park, Chan-Sik;Lee, Sang-Jeong
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.61.1-61
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    • 2001
  • This paper describes an efficient ambiguity searching method using additional constraints in 3-dimentional attitude finding GPS receiver design. For determining the integer ambiguity, the baseline length constraint, the angle constraint, the velocity constraint and the attitude constraint can be used for reducing the searching space. This paper describes the searching space algebraically and graphically. It is confirmed that the described restrictions are reasonable and the speed and the probability of ambiguity fixing are improved when the restricted searching spaces are applied Moreover, it is possible to design receivers of better quality by applying the method proposed in this paper.

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GPS를 이용한 자세결정에서 Unscented Kalman Filter를 이용한 성능 향상 (Performance Improvement in GPS Attitude Determination Using Unscented Kalman Filters)

  • 천세범;이은성;강태삼;지규인;이영재
    • 제어로봇시스템학회논문지
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    • 제11권7호
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    • pp.621-626
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    • 2005
  • With precise GPS carrier positioning result, we can get attitude information if GPS antenna has adequate attaching position on the vehicle. In this case, baseline length information can be bandied as an additional measurement or constraint. In this paper, we have proposed a method to improve the attitude accuracy. To overcome nonlinearity of baseline observation model, we analyze attitude estimation result using existing estimation method like a least square method and Kalman filter, and apply a new nonlinear estimation method an unscented Kalman filter Finally we confirm the improvement of attitude estimation result in the case of appling the unscented Kalman filter.

GPS 상시관측소 동적 좌표추정을 위한 중기선해석 정확도의 실험적 분석 (Experimental Assessment on Accuracy of Kinematic Coordinate Estimation for CORS by GPS Medium-range Baseline Processing Technique)

  • 조인수;이흥규
    • 한국측량학회지
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    • 제34권1호
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    • pp.79-90
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    • 2016
  • 본 논문에서는 지진 등으로 인해 발생하는 절대 지각변위 추정에 GPS 상시관측망의 동적기선해석 기법의 적용 가능성을 실험을 통해 정확도와 정밀도 측면에서 분석하였다. 국내 관측소의 절대좌표 추정을 위해 국외 관측소가 데이터처리에 포함 할 필요가 있어 실험 네트워크는 관측점 사이 거리가 수 백 ∼ 약 1,000km에 달하는 중기선으로 구성하였다. 따라서 대상 관측점의 동적 거동특성을 매개변수 추정단계에 반영하는 일련의 절차를 적용하여 GPS 동적 중기선해석 실험을 수행하였다. 이를 통하여 GPS 동적 중기선해석을 통해 센티미터 수준의 정확도와 그 이상의 정밀도로 GPS 상시관측소의 절대좌표를 동적모드로 추정할 수 있음을 확인하였다. 또한 본 논문은 위성궤도력, 관측데이터양 그리고 동적좌표 추정의 초기좌표 구속범위와 같은 기선해석 조건들이 동적좌표 추정 정확도와 정밀도에 미치는 영향을 분석하고 그 결과를 요약하고 있다.

ModelCenter를 이용한 QTP-UAV 프롭로터 블레이드 형상 최적설계 (Design Optimization of QTP-UAV Prop-Rotor Blade Using ModelCenter)

  • 강희정
    • 항공우주시스템공학회지
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    • 제11권4호
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    • pp.36-43
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    • 2017
  • 쿼드틸트 무인기에 적용되는 프롭로터 블레이드 형상 최적설계를 수행하였다. 형상 최적설계 프로세스 통합은 ModelCenter(R) 프로그램을 이용하였으며, 최적설계 과정에서 성능해석은 CAMRAD-II를 사용하였다. 목적함수는 제자리비행 및 전진비행 모드에서 성능효율 최대화로 설정하였으며, 제한조건은 소요 동력 및 피치로드 하중 값이 기본 형상 값보다 작게 되도록 설정하였다. 설계변수로는 블레이드 루트 코드길이, 테이퍼비, 비틀림 각의 기울기 및 각도, 하반각, 끝단 형상 생성을 위한 파라볼릭 계수, 하반각과 끝단형상이 적용되는 블레이드 스팬위치, 블레이드 단면을 구성하는 익형의 위치로 구성하였다. 최적 설계 결과 기준 형상 대비 제자리비행 효율은 1.6%, 전진 비행 효율은 13.6% 향상된 프롭로터 블레이드 형상을 도출할 수 있었으며, 피치로드 하중은 약 30% 감소하였다.

GPS 반송파 위상을 이용한 정밀 자세 측정 (Precise attitude determination using GPS carrier phase measurements)

  • 박찬식;이장규;지규인;이영재
    • 제어로봇시스템학회논문지
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    • 제3권6호
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    • pp.602-612
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    • 1997
  • With GPS carrier phase measurements from more than two antenna which attached to the vehicle, precise attitude can be easily obtained if the integer ambiguity included in carrier phase measurement is resolved. Recently some special products which use dual frequencies or has one receiver engine with multiple antenna are announced. But there are still strong requirements for the conventional single frequency off-the-shelf receiver. To meet these requirements, an efficient integer ambiguity resolution technique is indispensable. In this paper, a new technique to resolve integer imbiguity with single frequency receivers is proposed. The proposed method utilize the known baseline length as a constraint of independent elements of integer ambiguities. With this constraints, the size of search volume can be greatly reduced. Thus the true integer ambiguity can be easily determined with less computational burden and number of measurements. The proposed method is applied to real data to show its effectiveness.

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