• Title/Summary/Keyword: air force

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Development of CanSat System for Vehicle Tracking based on Jetson Nano (젯슨 나노 기반의 차량 추적 캔위성 시스템 개발)

  • Lee, Younggun;Lee, Sanghyun;You, Seunghoon;Lee, Sangku
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2022.10a
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    • pp.556-558
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    • 2022
  • This paper proposes a CanSat system with a vehicle tracking function based on Jetson Nano, a high-performance small computer capable of operating artificial intelligence algorithms. The CanSat system consists of a CanSat and a ground station. The CanSat falls in the atmosphere and transmits the data obtained through the installed sensors to the ground station using wireless communication. The existing CanSat is limited to the mission of simply transmitting the collected information to the ground station, and there is a limit to efficiently performing the mission due to the limited fall time and bandwidth limitation of wireless communication. The Jetson Nano based CanSat proposed in this paper uses a pre-trained neural network model to detect the location of a vehicle in each image taken from the air in real time, and then uses a 2-axis motor to move the camera to track the vehicle.

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Modeling of Linear Switched Reluctance Motor for Self Levitation and Propulsion (자기부상/추진 일체화를 위한 선형 스위치드 릴럭턴스 모터의 모델링)

  • Sung, So-Young;Cho, Han-Wok;Sung, Ho-Kyoung;Jang, Seok-Myung
    • Proceedings of the KIEE Conference
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    • 2007.10c
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    • pp.95-97
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    • 2007
  • This paper proposes a mathematical modelling about Leviation Force and Propulsion Force in a system, where Primary and Secondary LSRM air-gap is irregular. This can be a suitable model for Magnetically levitation Train, where Primary and Secondary air-gap mechanically has to control simultaneously Levitation Force and Propulsion Force.

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Nonlinear Vibration Analysis of Cantilever Beam Subject to Electromagnetic Force (전자력을 받는 외팔보의 비선형진동)

  • 최연선;서경석;우영주
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.05a
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    • pp.283-288
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    • 2001
  • The nonlinear vibration of a cantilever beam due to electromagnetic force is studied. The dynamic responses of the beam show various phenomena with the variation of the system parameters, such as jump phenomenon, multiple solutions and the change of the natural frequency. The nonlinear stiffness due to electromagnetic forces which depends on air gap size is measured experimentally. This system was modeled by a single degree of freedom nonlinear dynamic system and solved numerically for the system parameters. The numerical results show good agreements with the experimental observations, which demonstrates the nonlinearity of magnetic force.

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A Study of Dynamic Characteristic far Resistance Spot Welding Process Using Servo-gun System (서보건 이용 시 저항 점 용접의 동특성 분석에 관한 연구)

  • Baek Jung-Yeub;Lee Jong-Gu;Rhee Se-Hun
    • Journal of Welding and Joining
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    • v.23 no.3
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    • pp.40-46
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    • 2005
  • Air gun has been one of the good tools to press two sheet metals. However, it is not easy to control the acting force precisely. A Servo-gun is a good tool to control the acting force on the workpiece comparing with the air gun. Servo-gun has a higher tensile shear strength and lower indentation depth as well as smaller spatter. Dynamic resistance was obtained according to the acting force and welding current. As the acting force was changed during welding, the welding quality was increased.

Development of a Classification Model for Driver's Drowsiness and Waking Status Using Heart Rate Variability and Respiratory Features

  • Kim, Sungho;Choi, Booyong;Cho, Taehwan;Lee, Yongkyun;Koo, Hyojin;Kim, Dongsoo
    • Journal of the Ergonomics Society of Korea
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    • v.35 no.5
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    • pp.371-381
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    • 2016
  • Objective:This study aims to evaluate the features of heart rate variability (HRV) and respiratory signals as indices for a driver's drowsiness and waking status in order to develop the classification model for a driver's drowsiness and waking status using those features. Background: Driver's drowsiness is one of the major causal factors for traffic accidents. This study hypothesized that the application of combined bio-signals to monitor the alertness level of drivers would improve the effectiveness of the classification techniques of driver's drowsiness. Method: The features of three heart rate variability (HRV) measurements including low frequency (LF), high frequency (HF), and LF/HF ratio and two respiratory measurements including peak and rate were acquired by the monotonous car driving simulation experiments using the photoplethysmogram (PPG) and respiration sensors. The experiments were repeated a total of 50 times on five healthy male participants in their 20s to 50s. The classification model was developed by selecting the optimal measurements, applying a binary logistic regression method and performing 3-fold cross validation. Results: The power of LF, HF, and LF/HF ratio, and the respiration peak of drowsiness status were reduced by 38%, 22%, 31%, and 7%, compared to those of waking status, while respiration rate was increased by 3%. The classification sensitivity of the model using both HRV and respiratory features (91.4%) was improved, compared to that of the model using only HRV feature (89.8%) and that using only respiratory feature (83.6%). Conclusion: This study suggests that the classification of driver's drowsiness and waking status may be improved by utilizing a combination of HRV and respiratory features. Application: The results of this study can be applied to the development of driver's drowsiness prevention systems.

Comparison and Validation Study on Computational Fluid Dynamics and Wind Tunnel Test Results of Standard Dynamics Model (표준 동안정 모델의 전산유체해석 및 풍동시험 결과 비교검증)

  • Cho, Donghyurn;Kim, Seung Pil;An, Eunhye;Choi, Younseok;Roh, Jisoo;Chung, Hyoung Seog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.3
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    • pp.217-225
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    • 2017
  • This research represents comparison and validation of static aerodynamic results in different wind tunnel organizations and EFD-CFD results. KAFA conducted wind tunnel tests with Standard Dynamics Model(SDM) which is based on the NRC model, the same configuration of KARI; and then compared and analyzed similarities and differences of the data from KARI and NRC results for verifying the accuracy of wind tunnel tests. Also, We compared the result of CFD with that of wind tunnel tests and examined strakes effect in static characteristics which are attached on the forward fuselage of SDM for investigating the cause of some discrepancies. From this analysis, there are some discrepancies in Cm tendency between EFD-CFD and it did not show the big difference of aerodynamic characteristics by strake effects. Thus, we need to research additionally for analyzing the different cause of some discrepancies such as vortex structures by the rear strut or intake of SDM and regenerating grid resolution of CFD.

A Study on the Dynamic Characteristics of Air Foil Bearings Using LS(Least Square)/IV(Instrumental Variable) Method (LS/IV 기법을 이용한 공기 포일 베어링의 동특성 계수에 관한 연구)

  • Jo, Jun-Hyeon;Ryu, Keun;Kim, Chang-Ho;Lee, Yong-Bok
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.11a
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    • pp.677-684
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    • 2004
  • This paper describes a method for identifying the dynamic characteristics of air foil bearings for high speed turbomachinerys with the LS/IV method. In fact identifying the characteristics of air foil bearings is very difficult work, and it is tried to identify it. Experiments were conducted to determine the structural dynamic and hydrodynamic characteristics of air foil bearings. Numerical predictions compare the static and dynamic force performances. The housing of the bearing on the journal was driven by the impact hammer which were used to simulate impact force acting on air foil bearings. The characteristics of air foil bearings were extracted from the frequency response function (FRF) by LS(Least Square) method and IV(Instrumental Variable) method. The experiment was tested at 0 rpm and $10000\sim16000rpm$. And the test results were introduced about the dynamic characteristics of air foil bearings, and also compared with theoritical results.

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Study on the Noise Reduction in the Rotary Compressor Using BLDC Motor (BLDC 모터를 적용한 로터리 컴프레서 소음 저감에 관한 연구)

  • Kim, Jin-Soo;Lim, Kyung-Nae;Ku, Se-Jin;Lee, Jang-Woo;Jeon, Si-Moon
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.18 no.9
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    • pp.920-929
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    • 2008
  • The main noise and vibration source of the BLDC rotary compressor for air conditioner was analyzed by using the measurement of noise and vibration, noise contour, and experimental modal analysis. The source is presumed to the mechanical resonance excited by the electromagnetic attractive force of the BLDC motor. To reduce the excessive noise of the BLDC rotary compressor due to the mechanical resonance, air-gap enlargement and structural dynamic modification were applied in this paper. Its validations were conducted by the analysis of the electromagnetic attractive force which is generated by the BLDC motor and by the measurement of noise and vibration of the BLDC rotary compressor. By enlarging the length of air-gap and conducting the structural dynamic modification, the noise and vibration in the compressor was significantly improved by 4.5 dB(A) and 56 percent, respectively.

Analysis of DGPS Approach and Landing Accuracy using Air Base Precision Approach Radar (비행기지 PAR을 이용한 DGPS 공항 접근 및 착륙 정확도 분석)

  • Koo, Jung;Pyo, Sang-Ho;Kang, Kyeong-Sung;Kim, Ki-Hyung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.5
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    • pp.788-797
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    • 2011
  • This paper analyzes the accuracy on the approach and landing of aircraft to an airport through comparison with airbase Precision Approach Radar and aircraft track data of DGPS equipped in aircraft. The proposed analysis result could be a basis for verifying the possibility that DGPS can be utilized in Airbase precision approach and landing. Position identification capability of widely used commercial DGPS is fairly accurate on latitude and longitude, while there is a slight error for being used in an airbase accurate approach and landing of Category I precision when it comes to altitude. Thus, we tested accuracy by analyzing actual flight track data of high performance aircraft to verify the accuracy of the airbase approach and landing using DGPS. Through the research, we developed instrumentation to compare PAR track data with DGPS track data, which can be used in reducing the number of PAR verification Flight utilizing it as a system measuring PAR accuracy at PAR installation phase.

Research on the motion characteristics of a trans-media vehicle when entering water obliquely at low speed

  • Li, Yong-li;Feng, Jin-fu;Hu, Jun-hua;Yang, Jian
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.10 no.2
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    • pp.188-200
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    • 2018
  • This paper proposes a single control strategy to solve the problem of trans-media vehicle difficult control. The proposed control strategy is just to control the vehicle's air navigation, but not to control the underwater navigation. The hydrodynamic model of a vehicle when entering water obliquely at low speed has been founded to analyze the motion characteristics. Two methods have been used to simulate the vehicle entering water in the same condition: numerical simulation method and theoretical model solving method. And the results of the two methods can validate the hydrodynamic model founded in this paper. The entering water motion in the conditions of different velocity, different angle, and different attack angle has been simulated by this hydrodynamic model and the simulation has been analyzed. And the change rule of the vehicle's gestures and position when entering water has been obtained by analysis. This entering water rule will guide the follow-up of a series of research, such as the underwater navigation, the exiting water process and so on.