2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology最新文献_第2页

Attitude control of bias momentum micro satellite using magnetic and gravity gradient torque 基于磁重力梯度转矩的偏动量微卫星姿态控制

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024395

M. Mukhayadi, R. Madina, U. Renner

{"title":"Attitude control of bias momentum micro satellite using magnetic and gravity gradient torque","authors":"M. Mukhayadi, R. Madina, U. Renner","doi":"10.1109/ICARES.2014.7024395","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024395","url":null,"abstract":"Earth pointing satellites commonly use bias momentum for attitude control. It provides gyroscopic stability against the external disturbance torque. Typically, the bias momentum satellite use momentum wheel and thruster for actuator and star tracker or pairs of horizon and a sun sensor to determine the direction of angular momentum. This paper proposes an effective technique to control the angular momentum of Lapan-Tubsat satellite using wheels and magnetic coil for actuator and overcome the limitations of the spacecraft that has no on-board horizon sensor and magnetometer that usually used to measure the magnetic field. The determination of angular momentum direction use video camera instead a horizon sensor even though it is available once per 24 hours of ground station contact. This idea is effective if only the disturbance torque and the angular momentum has been characterized and established. After the video camera gives attitude information the satellite operator tries to control the direction of angular momentum by over or under-compensate the disturbance torque using magnetic coil. On Lapan-Tubsat, the disturbance torque level is in the order of 10-5 Nm, i.e. 10% of the maximum coil torque.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"98 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131825043","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 12

Wireless Sensor Networks for microclimate telemonitoring using ZigBee and WiFi 使用ZigBee和WiFi进行微气候远程监测的无线传感器网络

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024404

Firdaus, Ahriman, Rois Akbar, E. Nugroho

引用次数: 6

Design and implementation of LDPC(Low Density Parity Check) coding technique on FPGA (Field Programmable Gate Array) for DVB-S2 (Digital Video Broadcasting-Satellite) 基于FPGA的DVB-S2数字视频广播卫星低密度奇偶校验(LDPC)编码技术的设计与实现

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024407

Rita Purnamasari, H. Wijanto, Iswahyudi Hidayat

引用次数: 2

A real-time monocular vision-based frontal obstacle detection and avoidance for low cost UAVs in GPS denied environment GPS拒绝环境下低成本无人机基于实时单目视觉的正面障碍物检测与避障

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024382

Saumajit Saha, A. Natraj, S. Waharte

引用次数: 47

Wavelet transform based new interpolation technique for satellite image resolution enhancement 基于小波变换的卫星图像分辨率增强插值新技术

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024405

P. Rasti, Iiris Lusi, H. Demirel, R. Kiefer, G. Anbarjafari

{"title":"Wavelet transform based new interpolation technique for satellite image resolution enhancement","authors":"P. Rasti, Iiris Lusi, H. Demirel, R. Kiefer, G. Anbarjafari","doi":"10.1109/ICARES.2014.7024405","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024405","url":null,"abstract":"In this research paper, we propose a new interpolation technique based on the Stationary Wavelet Transform (SWT) and iterative back projection (IBP) for satellite images. Firstly the low resolution image is interpolated by using bicubic interpolation and then decomposed into different subband images by SWT. Each subband is decimated to four lower low resolution images. The four low resolution images are interpolated and registered by using bicubic interpolation and IBP respectively. Inverse SWT (ISWT) is used to generate a Super-resolved output image. The proposed interpolation technique has been tested on several remote sensing images. The quantitative PSNR and SSIM results as well as the visual results show the superiority of the proposed interpolation technique over the other interpolation and image resolution enhancement techniques. For one of the images the PSNR of the proposed method has achieved 3.84dB, 2.11dB, and 1.1dB more improvements than bicubic interpolation, Irani and Peleg technique, and Wavlet Zero Padding technique respectively.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"74 4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128046117","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 18

ASIGN - Mission-critical visual communications for integrated space applications 用于综合空间应用的关键任务视觉通信

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024402

H. Skinnemoen

引用次数: 1

Development of transferable rule-sets for urban areas using QuickBird satellite imagery 利用QuickBird卫星图像为城市地区制定可转让的规则集

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024390

Anahita Tathiri, H. Shafri, Alireza Hamedianfar

引用次数: 0

Hexacopter outdoor flight test results of an Extended State Observer based controller 基于扩展状态观测器控制器的六旋翼机室外飞行试验结果

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024373

Christian D. Heise, Guillermo P. Falconi, F. Holzapfel

引用次数: 20

A utility aircraft for remote sensing missions with a high-precision automatic flight control system 一种具有高精度自动飞行控制系统的用于遥感任务的通用飞机

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024378

R. Luckner, L. Dalldorff, R. Reichel

{"title":"A utility aircraft for remote sensing missions with a high-precision automatic flight control system","authors":"R. Luckner, L. Dalldorff, R. Reichel","doi":"10.1109/ICARES.2014.7024378","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024378","url":null,"abstract":"Light civil utility aircraft are well suited for remote sensing missions and to serve as an airborne platform for efficient reconnaissance, surveillance, exploration, and measurement tasks in a growing market. Missions where the pilot has to operate a payload require an automatic flight control system (AFCS) to support the pilot. In missions that are extremely difficult, long or dangerous, the AFCS may even replace the pilot. Such an AFCS has to follow precisely predefined trajectories and should compensate disturbances due to atmospheric turbulence. For un-manned aircraft operations it has to have full authority, it has to be highly reliable, and it must be able to take off and land automatically. The development and certification of such an AFCS at competitive cost is a major challenge. This paper gives an overview on the STEMME S15 utility aircraft, for which an AFCS has been developed. It describes the design objectives, the selected flight control architecture, the system, and the flight test equipment as well as flight test results that demonstrate the high precision of flight path control.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"55 2","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114012363","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 5

The development of multi-band equatorial orbiting POLSAR satellite sensors 多波段赤道轨道POLSAR卫星传感器的研制

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024384

W. Boerner

{"title":"The development of multi-band equatorial orbiting POLSAR satellite sensors","authors":"W. Boerner","doi":"10.1109/ICARES.2014.7024384","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024384","url":null,"abstract":"With the relentless increase in population density, the anthropogenic expansion into natural terrestrial hazard zones has become irreversible resulting in ever more catastrophic disasters especially within the entire tropical belts engulfing Mother Earth. What is required is around-the-clock local and wide-area surveillance and remote sensing of the vegetative cover for which hitherto well designed optical equatorial orbiting satellite sensors had been developed but their successful implementation is failing ever more because of the ever increasing cloud, precipitation, humidity and increasing aerosol cover within the entire equatorial belt of +/- 15°-20° latitude rendering penetration at optical wavelength mostly ineffective. Hence, recourse must be taken of active microwave sensing, and implementing radar and synthetic aperture sensors from air and space operational at day & night and which are mainly independent of weather: The sensors especially suited are the fully polarimetric POL-SAR sensors developed for satellite remote sensing by the major SAR technology development centres worldwide. The challenge is thus to develop equatorial orbiting SAR, preferably wide-swath POL-SAR satellite sensors, within the desirable P/L/S/C/X/Ka multi-bands by implementing novel beam-steering radar for wide-swath high-resolution coverage. Therefore, we need to mobilize and draw full responsible attention of the main SAR Development Centres and its Supporting Organizations worldwide in order for realizing the challenging proposal.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"320 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122804048","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 4