• 한국약용작물학회:학술대회논문집
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• 한국약용작물학회 2011년도 춘계학술발표회
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• pp.152-153
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• 2011

• 제어로봇시스템학회논문지
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• 제7권11호
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• pp.944-952
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• 2001

Inertial navigation system(INS) errors increase with time due to inertial sensor errors, and therefore it is desired to combine INS with external aids such as GPS. However GPS informations have a randomly abrupt jump due to a sudden corruption of the received satellite signals and environment, and moreover GPS can\`t provide navigation solutions. In this paper, smoothing and prediction schemes are proposed for GPS`s jump or unavailable GPS. The smoothing algorithm which is designed as a scalar adaptive filter, smooths abrupt jump. The prediction algorithm which is proved by Schuler error model of INS, estimates INS error in appropriate time. The outputs of proposed algorithm apply stable measurements to GPS aided INS Kalman filter. Simulations show that the proposed algorithm can effectively remove measurement jump and predict INS error.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.133.1-133
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• 2001

When the signals from satellite vehicles are blocked, it is impossible to provide positioning information. Integrating CDGPS with INS, the performances of output can be greatly improved. In the CDGPS/INS integrated system, the error growth in INS can be efficiently suppressed due to CDGPS. On the contrary, the search range of integer ambiguities can be reduced with the aids of INS. Furthermore, cycle slips in carrier phase measurements can be easily detected using INS. The paper presents a CDGPS/INS integrated system that utilizes CDGPS aided with INS. Using the outputs of CDGPS/INS integration filter, a method to reduce search range of integer ambiguities is proposed. A method to detect cycle slips in carrier phase measurements is ...

• Journal of information and communication convergence engineering
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• 제5권3호
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• pp.289-294
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• 2007

With regard to a marine safety system, large vessels are generally loaded with INS (Integrated Navigation System). But although small and medium-sized ships are exposed to safety accidents in the sea, they are not carrying proper navigation devices and equipment. Accordingly, in order to develop INS for small and medium-sized ships(s-INS), an existing INS has newly been organized and integrated. Recently, more strict enforcement of INS-related regulations is expected at home and abroad, and the scope of their applications is being broadened. To keep up with this global trend that ships are being loaded with digital devices and equipment, this study has tried to develop s-INS, broadening its applications, and suggesting a future research plan.

• 한국항행학회논문지
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• 제21권4호
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• pp.339-346
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• 2017

본 논문에서는 위성항법장치와 관성항법장치가 장착된 항체의 고속 이동을 모의하는 환경에서 재밍신호가 인가되었을 때, INS-aided 알고리즘이 장착된 위성항법장치의 재밍대응 성능향상을 검증하기 위한 관성항법장치 모의 장치의 설계 방안을 제시한다. 위성항법 시뮬레이터와 연동하여 관성데이터를 제공할 수 있는 고가의 관성항법장치 시뮬레이터를 대체하기 위해 상대적으로 낮은 가격으로 제작할 수 있는 관성항법장치 모의 장치 설계 방안을 제시하였다. 제안한 설계를 기반하여 제작한 모의 장치를 이용하여 INS-aided 알고리즘이 장착된 위성항법장치의 재밍대응 성능을 검증하기 위해 항체의 고속 이동 환경을 모의한 시험 환경을 구축하였다. 모의 시험을 통해 GPS L1 C/A와 L2C 항법신호에 인가되는 협대역/광대역의 재밍신호에 대응하여 INS-aided 알고리즘 미적용 시와 대비하여 기존 문헌에서 분석한 +5 dB의 재밍대응 성능 향상이 가능함을 확인하였다. 모의 시험 결과를 통해 본 논문에서 설계하여 제작한 관성항법장치 모의 장치가 재밍대응 성능향상 검증을 위한 관성데이터 주입이 가능함을 검증할 수 있었다.

• Journal of Positioning, Navigation, and Timing
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• 제4권3호
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• pp.141-150
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• 2015

In this study, a Global Navigation Satellite System (GNSS) / Inertial Navigation System (INS) / odometer / barometer integrated navigation system that uses a commercial navigation device including Micro Electro Mechanical Systems (MEMS) accelerometer and gyroscope in addition to GNSS, odometer information obtained from a vehicle, and a separate MEMS barometer sensor was implemented, and the performance was verified. In the case of GNSS and GNSS/INS integrated navigation system that are generally used in a navigation device, the performance would deteriorate in areas where GNSS signals are not available. Therefore, an integrated navigation system that calculates a better navigation solution in areas where GNSS signals are not available compared to general GNSS/INS by correcting the velocity error of GNSS/INS using an odometer and by correcting the cumulative altitude error of GNSS/INS using a barometer was suggested. To verify the performance of the navigation system, a commercial navigation device (Softman, Hyundai Mnsoft, http://www.hyundai-mnsoft.com) and a barometer sensor (ST Company) were installed at a vehicle, and an actual driving test was performed. To examine the performance of the algorithm, the navigation solutions of general GNSS/INS and the GNSS/INS/odometer/barometer integrated navigation system were compared in an area where GNSS signals are not available. As a result, a navigation solution that has a smaller position error than that of GNSS/INS could be obtained in the area where GNSS signals are not available.

• 대한공간정보학회지
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• 제16권1호
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• pp.43-48
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• 2008

본 연구에서는 GPS/INS 항공사진측량 기술을 이용하여 1/1,000 수준의 대축척 수치지형도를 제작하고 전통적인 항공사진측량과의 차이점, 즉 정확도, 경제성 등을 평가하여 GPS/INS 항측의 효율성을 평가하였다. 연구결과, 지상 기준점측량 공정에서 약 40%의 작업량 절감효과가 발생한 것으로 나타났으며, 작업지역의 크기에 따른 작업효율성은 1/5,000 항측의 경우 전통적인 방법과 동일한 정확도를 유지하는 것을 기준으로 할 때 대략 10모델과 20모델 블록에서는 55%, 30모델 블록의 경우 60%의 지상기준점이 감소함을 확인하였다.

• 한국약용작물학회:학술대회논문집
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• 한국약용작물학회 2011년도 추계학술발표회
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• pp.132-133
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• 2011

• 한국약용작물학회:학술대회논문집
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• 한국약용작물학회 2010년도 심포지엄 및 추계학술발표회
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• pp.197-198
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• 2010

• 한국약용작물학회:학술대회논문집
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• 한국약용작물학회 2010년도 심포지엄 및 추계학술발표회
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• pp.205-206
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• 2010