2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology最新文献

Modular trajectory / path following controller using nonlinear error dynamics 采用非线性误差动力学的模块化轨迹/路径跟踪控制器

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024374

Simon P. Schatz, F. Holzapfel

引用次数: 39

Reference command shaping for approximate dynamic inversion based model Reference Adaptive Control 基于近似动态反演模型的参考命令整形参考自适应控制

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024377

Maximilian Muhlegg, P. Niermeyer, F. Holzapfel

{"title":"Reference command shaping for approximate dynamic inversion based model Reference Adaptive Control","authors":"Maximilian Muhlegg, P. Niermeyer, F. Holzapfel","doi":"10.1109/ICARES.2014.7024377","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024377","url":null,"abstract":"A hybrid adaptive-optimal control architecture is presented, which is suitable for implementation on systems with fast, nonlinear and uncertain dynamics subject to constraints. Approximate dynamic inversion transforms the nonlinear system into an equivalent linear form. A linear error controller allows a designer chosen reference model to be tracked by the inverted plant. Model Reference Adaptive Control uses a weighted combination of basis functions in order to reduce the impact of modeling uncertainties on the closed loop dynamics. The underlying assumption is, that if the uncertainty is cancelled, the plant behaves like the inversion model and tracks the reference model exactly. Reference models are often chosen to be conservative. By employing a Model Predictive Controller to shape the reference command, the full control authority of the plant can be exploited, while simultaneously abiding input and state constraints. Since the reference model is preselected, the optimal control problem can be solved offline, drastically reducing the onboard required computational power. The control architecture is implemented for the attitude loop of a multirotor system and validated in flight test.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"7 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":"117106764","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

Generic study of solar radiation and solar wind sailing 太阳辐射和太阳风航行的一般研究

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024386

H. Djojodihardjo, A. Yousefian, R. Ahmed

引用次数: 1

Evaluation of soil erosion potential of a hilly terrain using hypsometry and E30 model: A case study of Kynshi Basin, Meghalaya 基于拟测法和E30模型的丘陵地形土壤侵蚀潜力评价——以梅加拉亚邦Kynshi盆地为例

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024393

N. Sinha, D. Deb, K. Pathak

{"title":"Evaluation of soil erosion potential of a hilly terrain using hypsometry and E30 model: A case study of Kynshi Basin, Meghalaya","authors":"N. Sinha, D. Deb, K. Pathak","doi":"10.1109/ICARES.2014.7024393","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024393","url":null,"abstract":"Watersheds in hilly terrain are prone to severe erosion due to surface runoff, steep slopes and undulating topography. Kynshi watershed, situated in west Khasi Hills district of Meghalaya in India, is vulnerable to soil erosion due to heavy rainfall, its high elevation and undulating terrain. However, the area is covered with dense to moderate forest which may act as deterrent to erosion. This study evaluates the soil erosion potential of the watershed by hypsometric analysis and Remote Sensing and GIS based E30 model. Results suggest that a significant area (almost 41%) faces soil erosion at a rate of 0-22.25 mm/yr and about 9.5% area may suffer from an erosion rate of above 66.75 mm/yr. The area is inaccessible for any field measurements and hence erosion values estimated in this study could not be validated. However, study forecasts pattern of soil erosion in the area while hypsometric study shows that the watershed is at a mature stage of erosion having low erodibility. Since land cover may change due to anthropogenic activities, it can induce higher erosion potential.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"16 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":"126365565","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: 1

Position tracking of a hexacopter using a geometric backstepping control law - Experimental results 基于几何反步控制律的六旋翼机位置跟踪实验结果

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024375

Guillermo P. Falconi, F. Holzapfel

引用次数: 11

Multi mission low earth orbit equatorial satellite for Indonesian regions 印尼地区多任务近地轨道赤道卫星

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024394

E. N. Nasser

{"title":"Multi mission low earth orbit equatorial satellite for Indonesian regions","authors":"E. N. Nasser","doi":"10.1109/ICARES.2014.7024394","DOIUrl":"https://doi.org/10.1109/ICARES.2014.7024394","url":null,"abstract":"Low earth orbit (LEO) equatorial satellite has become a favorable option for developing countries like Indonesia. Low propagation delay, low transmission power and also low cost in term of satellite development and launch are the main attraction of the LEO satellite system. In this paper, we propose multi mission satellite LEO equatorial satellite for telecommunication, surveillance and vessel monitoring based on AIS (Automatic Identification System). First iteration was the tradeoff between communication payload mission and other missions in defining the orbit constellation type and altitude. Simulation was done for orbit constellation, orbit environment, antenna pattern, and coverage analysis. The simulation result will become input for link budget calculation, ITU constraint (PFD and EPFD) and handover mechanism scheme selection. The result shows that single plane 1500 km LEO equatorial with 14 satellites was able to provide dual satellite diversity for all Indonesian region. It also shows that C-band and Ku-band Frequency will exceed the EPFD limit with 10 dbi antenna gain and 30 W transmit power. The optimum configuration of Ext C-band with hemispherical patch antenna shows that the minimum fading margin > 1 dB is required to implement the hard handover scheme.","PeriodicalId":159808,"journal":{"name":"2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology","volume":"66 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":"124131371","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: 8

Optimal trajectories for RPAS with discrete controls and discrete constraints 具有离散控制和离散约束的RPAS的最优轨迹

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024372

M. Rieck, M. Richter, M. Bittner, F. Holzapfel

引用次数: 0

Novel two position ground alignment technique for Strapdown Inertial Navigation System 捷联惯导系统两位置地面对准新技术

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024389

R. B. Sri, Reddy B. Venugopal, R. S. Chandrasekhary, Bhvs Narayana Murthy

引用次数: 4

Real-time simulation of nonlinear transmission behavior in electro-mechanical flight control systems 机电飞行控制系统非线性传输行为的实时仿真

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024380

Patrick J. Lauffs, Markus Hochstrasser, F. Holzapfel

引用次数: 3

UAV & satellite communications live mission-critical visual data 无人机和卫星通信实时任务关键视觉数据

2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology Pub Date : 2014-11-01 DOI: 10.1109/ICARES.2014.7024391

H. Skinnemoen

引用次数: 29