• Advances in aircraft and spacecraft science
• /
• 제7권1호
• /
• pp.1-17
• /
• 2020

In this paper, a new model-based Fault Detection and Diagnosis (FDD) method for an agile supersonic flight vehicle is presented. A nonlinear model, controlled by a classical closed loop controller and proportional navigation guidance in interception scenario, describes the behavior of the vehicle. The proposed FDD method employs the Inertial Navigation System (INS) data and nonlinear dynamic model of the vehicle to inform fins damage to the controller before leading to an undesired performance or mission failure. Broken, burnt, unactuated or not opened control surfaces cause a drastic change in aerodynamic coefficients and consequently in the dynamic model. Therefore, in addition to the changes in the control forces and moments, system dynamics will change too, leading to the failure detection process being encountered with difficulty. To this purpose, an equivalent aerodynamic model is proposed to express the dynamics of the vehicle, and the health of each fin is monitored by the value of a parameter which is estimated using an adaptive robust filter. The proposed method detects and isolates fins damages in a few seconds with good accuracy.

• 대한원격탐사학회지
• /
• 제23권5호
• /
• pp.365-373
• /
• 2007

Car navigation system is a key application in geographic information system and telematics. A recent trend of car navigation system is using real video captured by camera equipped on the vehicle, because video has more representation power about real world than conventional map. In this paper, we suggest a visual car navigation system that visually represents route guidance. It can improve drivers' understanding about real world by capturing real-time video and displaying navigation information overlaid directly on the video. The system integrates real-time data acquisition, conventional route finding and guidance, computer vision, and augmented reality display. We also designed visual navigation controller, which controls other modules and dynamically determines visual representation methods of navigation information according to current location and driving circumstances. We briefly show implementation of the system.

• 한국군사과학기술학회지
• /
• 제11권2호
• /
• pp.66-72
• /
• 2008

A distributed missile system is composed of command control center, radar and launcher which exchange information each other to use wire or wireless network. The distributed missile system is required mobility for operational convenience and survivability. Also missile system requests land navigation system to provide relatively accurate attitude. For reason of these requirements, each subsystem needs land navigation which provides information of position and attitude. This paper represents operational concept for land navigation to consider operational environment and concrete operational procedure to apply the operational concept. In state that there is no operation for land navigation of distributed missile system internally so for, this paper could be helped to establish operational concept and procedure of this kind of system.

• 대한공간정보학회지
• /
• 제2권2호
• /
• pp.81-88
• /
• 1994

CNS(Car Navigation System)는 국내외적으로 자율주행차량(Autonomous Land Vehicle)연구분야에서 주행계획 용도보다는 일반차량에서 운전자 보조 시스템으로 더 많이 쓰이고 있다. 본 논문에서는 CNS에 한 연구분야인 Global Path Planning의 새로운 위치추적 알고리즘 결과를 개발하였다. 일본과 같은 경우에는 벌써 이러한 CNS의 연구가 활발히 진행되어서 현재는 상품화되어 년간 $40{\sim}50$만개 정도가 팔리고 있고 미국 및 유럽 각국(EC)에서도 CNS의 개발 및 상품화가 활발히 진행되고 있다. 우리나라의 경우엔 아직 주행중인 차량의 현재위치를 구하고 이를 Digital Map상에 실시간으로 구현하는 제 1세대 CNS가 연구 중에 있으나 아직은 초기 단계에 있다. 이에 본 논문은 현재까지 우리나라에서 연구중인 인공위성과 범지구적 위치결정체계(Global Positioning System)만을 이용한 차량 위치 추정 방법에 추측항법체계(Dead_Reckoning)라는 다른 방법을 결합하여 기존의 차량 위치 추정 오차를 줄여주는 새로운 알고리즘을 제시하고 실제차량에서의 실험결과를 보인다.

• 한국항해항만학회지
• /
• 제37권3호
• /
• pp.309-313
• /
• 2013

본 연구는 복합센서를 활용한 무인지게차의 주행 시스템에 대한 것이다. 무인지게차가 화물 이 적재를 위해 랙에 진입할 시 필요한 주행기술로 무인지게차의 위치 및 방향을 정확하게 파악하기 위해 RFID, IMU센서 및 근접센서로 구성된 복합센서 시스템을 이용하였고, 각 센서의 성능실험을 통해 특성을 파악한다. 이를 직접 설계/제작한 실험용 차량에 부착하여 복합센서 시스템을 적용하는 실험을 수행하고 이를 통해 개발된 시스템의 성능을 검증하였다.

• Journal of Mechanical Science and Technology
• /
• 제19권8호
• /
• pp.1529-1543
• /
• 2005

Recently an unmanned aerial vehicle (UAV) has been widely used for military and civil applications. The role of a navigation system in the UAV is to provide navigation data to the flight control computer (FCC) for guidance and control. Since performance of the FCC is highly reliant on the navigation data, a fault in the navigation system may lead to a disastrous failure of the whole UAV. Therefore, the navigation system should possess a fault detection and isolation (FDI) algorithm. This paper proposes an attitude determination GPS/INS integrated navigation system with an FDI algorithm for a UAV. Hardware for the proposed navigation system has been developed. The developed hardware comprises a commercial inertial measurement unit (IMU) and the integrated navigation package (INP) which includes an attitude determination GPS (ADGPS) receiver and a navigation computer unit (NCU). The navigation algorithm was implemented in a real-time operating system with a multi-tasking structure. To evaluate performance of the proposed navigation system, a flight test has been performed using a small aircraft. The test results show that the proposed navigation system can give accurate navigation results even in a high dynamic environment.

• 대한공간정보학회지
• /
• 제4권1호
• /
• pp.103-114
• /
• 1996

이동체 통제 시스템은 자동차 항법 시스템(Car Navigation Systm)과 GIS(Geographical Information System), 통신망 등을 결합하여 중앙통제실에서 동적으로 이동체들의 위치를 감지하고, 이를 종합적으로 관리하는 시스템이다. 따라서, 이동체 통제 시스템은 신속한 순찰차의 이동이나 화물 수송 등을 실시간에 통제할 수 있다. 본 논문에서는 이동체 통제 시스템과 같이 도로 데이타, 이동체 데이타, 이동체의 위치 데이타 등을 다루는 응용 시스템의 개발을 위한 데이타 관리자를 설계하고 구현하였다. 본 논문에서 제안하는 데이타 관리자는 크게 시스템 관리 모듈, 도로 데이타 관리 모듈, 이동체 데이타 관리 모듈, GPS 데이타 관리 모듈, 부가정보 데이타 관리 모듈로 구성되어 있다. 그리고, 저장 시스템으로는 미국 위스콘신 대학에서 개발하고 있는 SHORE(Scalable Heterogeneous Object REpository) 베타 0.9.3 버젼의 저장 관리자를 사용하였다.

• 한국항해항만학회지
• /
• 제35권2호
• /
• pp.121-130
• /
• 2011

The localization of vehicle is an important part of an unmanned vehicle control problem. Pseudolite ultrasonic system(PUS) is the method to find an absolute position with a high accuracy by using ultrasonic sensor. And Gyro is the inertial sensor to measure yaw angle of vehicle. PUS can be able to estimate the position of mobile robot precisely, in which errors are not accumulated. And Gyro is a more faster measure method than PUS. In this paper, we suggest a more accuracy method of calculating PUS which is numerical analysis approach named Newtonian method. And also propose the fusion method to increase the accuracy of estimated angle on moving vehicle by using PUS and Gyro integrated system by Kalman filtering. To control the 4WS unmanned vehicle, the trajectory following algorithm is suggested. And the new concept arbitration of goal controller is suggested. This method considers the desirability function of vehicle state. Finally, the performances of Newtonian method and designed controller were verified from the experimental results with the 4WS vehicle scaled 1/10.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2005년도 ICCAS
• /
• pp.1867-1870
• /
• 2005

The celestial navigation is one of alternatives to GPS system and can be used as a backup of GPS. In the celestial navigation system using more than two star trackers, the vehicle's ground position can be solved based on the star trackers' attitude information if the vehicle's local vertical or horizontal angle is given. In order to determine accurate ground position of flight vehicle, the high accurate local vertical angle measurement is one of the most important factors for navigation performance. In this paper, the Earth geophysical deflection was analyzed in the assumption of using the modern electrolyte tilt sensor as a local vertical sensor for celestial navigation system. According to the tilt sensor principle, the sensor measures the tilt angle from gravity direction which depends on the Earth geoid surface at a given position. In order to determine the local vertical angle from tilt sensor measurement, the relationship between the direction of gravity and the direction of the Earth center should be analyzed. Using a precision orbit determination software which includes the JGM-3 Earth geoid model, the direction of the Earth center and the direction of gravity are extracted and analyzed. Appling vector inner product and cross product to the both extracted vectors, the magnitude and phase of deflection angle between the direction of gravity and the direction of the Earth center are achieved successfully. And the result shows that the angle differences vary as a function of latitude and altitude. The maximum 0.094$^{circ}$angle difference occurs at 45$^{circ}$latitude in case of 1000 Km altitude condition.

• 한국군사과학기술학회지
• /
• 제5권3호
• /
• pp.62-76
• /
• 2002

This paper describes the design of a Coordinates Tracking algorithm for EOTS and its error analysis. EOTS stabilizes the image sensors such as FLIR, CCD TV camera, LRF/LD, and so on, tracks targets automatically, and provides navigation capability for vehicles. The Coordinates Tracking algorithm calculates the azimuth and the elevation angle of EOTS using the inertial navigation system and the attitude sensors of the vehicle, so that LOS designates the target coordinates which is generated by a Radar or an operator. In the error analysis in this paper, the unexpected behaviors of EOTS that is due to the time delay and deadbeat of the digital signals of the vehicle equipments are anticipated and the countermeasures are suggested. This algorithm is verified and the error analysis is confirmed through simulations. The application of this algorithm to EOTS will improve the operational capability by reducing the time which is required to find the target and support especially the flight in a night time flight and the poor weather condition.