{"title":"A network architecture based on information, control and behavior definitions","authors":"H. Michel","doi":"10.1109/FBW.2010.5613794","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613794","url":null,"abstract":"This paper envisions a plug-and-play architecture that will allow engineers to rapidly and robustly define and configure wireless systems for aircraft operations. The architecture described here is based on a layered functional decomposition of the three aspects of operations: information flow, control flow and behavior. These individual layered decompositions are presented as an integrated technical reference model (I-TRM). Having an I-TRM is crucial to developing affordable and robust systems that are self-aware, self-healing and adaptable within a resource-constrained environment.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"38 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115768754","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}
{"title":"Impact localization and scaling for SHM of inflatable habitats","authors":"K. Schrader, A. Abedi, V. Caccese","doi":"10.1109/FBW.2010.5613793","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613793","url":null,"abstract":"This work focuses on the structural monitoring of an inflatable lunar habitat, more specifically, characterizing impacts on the surface of such a structure. Given the lack of an atmosphere, the moon is not shielded from small space debris that would normally incinerate on earth, creating the need for these additional safeguards. This project explores an accelerometer based system to localize and scale an impact on the structures surface. An inflatable testbed is setup with appropriately selected sensors and data collection hardware. Tailored for wireless sensor implementation, methodologies are developed that utilize the accelerometer array to accurately determine the location, and calculate the intensity of, an impacting object. Various approaches to the caveats of such a task are explored throughout. Finally, the resulting algorithms are tested and evaluated on the lunar habitat test structure, providing a working proof-of-concept for an accelerometer based wireless impact localization and scaling system‥","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"49 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133343181","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}
{"title":"Wireless cooperative relaying using game theory","authors":"F. Afghah, A. Razi, A. Abedi","doi":"10.1109/FBW.2010.5613786","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613786","url":null,"abstract":"Wireless systems have various applications in aerospace technologies including aircraft navigation system, and monitoring and control module. In wireless networks, specially for the range-limited transceivers, relaying systems are widely used to extend the reach of communication networks, increase throughput, and save on power. In most of relay networks, the source and relay nodes share the same radio channel to send data, so there is a competition among nodes to access the channel. In this article, a novel stochastic game theoretical model for cooperative packet forwarding is proposed to provide an efficient cooperation solution for nodes to achieve better power and throughput performance. The proposed method is based on the Markovian stationary game theoretical model with two players. Both cooperative and non cooperative solutions are provided.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"19 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133638353","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}
{"title":"Conceptual design study of a structural health monitoring system","authors":"Jérôme Pinsonnault, Wei Liu","doi":"10.1109/FBW.2010.5613797","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613797","url":null,"abstract":"This paper presents a global SHM architecture and an example of conceptual design study of a structural health monitoring system.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"18 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116631144","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}
{"title":"Hierarchical network development of wireless passive sensors","authors":"A. Razi, F. Afghah, A. Abedi","doi":"10.1109/FBW.2010.5613796","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613796","url":null,"abstract":"Design and implementation of wireless sensor systems is one of the important issues in aerospace technologies. It has wide range of applications such as monitoring different parameters in aircraft engines, satellites indoor and outdoor conditions as well as environmental data in moon and other planets in space exploration activities. In most of these applications, it is not possible to utilize active sensors due to operation failure in harsh conditions. In this article, design and implementation of a system consist of both active and passive sensors is studied.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"18 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114999765","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}
{"title":"Modeling and simulation of heterogeneous electronic system based on smart sensors with frequency acquisition for aerospace structural health monitoring","authors":"C. Ferrer, P. Álvarez, R. Aragonés, J. Oliver","doi":"10.1109/FBW.2010.5613791","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613791","url":null,"abstract":"This work presents a top-down design methodology for a behavioral modeling System, based on smart sensors for aerospace structures monitoring, implemented on a MATLAB/Simulink environment. The modeled acquisition platform in this aeronautic health monitoring systems (AHMS) is built using the following specific sensors: humidity, pressure, temperature, stress and acceleration. For this application it has been implemented frequency acquisition techniques ensuring optimum noise immunity, particularly: a signal acquisition technique based on voltage to frequency converter, capacitance to frequency and frequency to code converters (VtoF-cC, CtoF-cC). The Matlab-Simulink model presents a high accuracy level in signal acquisition and conditioning compared to the electrical system simulation behavior.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"34 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132753168","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}
{"title":"Coded wireless temperature sensors with design specified sensitivity","authors":"J. Hines, L. Solie","doi":"10.1109/FBW.2010.5613790","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613790","url":null,"abstract":"ASR&D has developed a patented surface acoustic wave (SAW) temperature sensor with individual sensor identification codes and design-controlled temperature sensitivity. Temperature sensitivities demonstrated during this work range from −165ppm/°C to +680 ppm/°C, all on YZ lithium niobate, a piezoelectric substrate with an inherent temperature sensitivity of magnitude 94ppm/°C. A set of 32 individually identifiable coded SAW temperature sensor devices were developed. Wireless measurements confirmed the ability to selectively detect any single sensor out of the combined response of multiple sensors. The wireless electronic reader system currently being developed at ASR&D is a single-channel reader that can be manually adjusted to select any one sensor out of a group of up to 32 sensors simultaneously operating in the field of view (FOV) of the reader. This system avoids code collision problems typical of prior coded SAW wireless sensor systems, and can be extended to read 32 or more sensors operating in the FOV of one reader, at ranges of up to 100 feet, with sampling times of 1–10 msec.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131398698","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}
Akihisa Matsubara, Tatsuya Ichikawa, A. Tomiki, T. Toda, Takehiko Kobayashi
{"title":"Experimental evaluation of ultra wideband wireless transmission within a spacecraft for replacing wired interface buses","authors":"Akihisa Matsubara, Tatsuya Ichikawa, A. Tomiki, T. Toda, Takehiko Kobayashi","doi":"10.1109/FBW.2010.5613795","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613795","url":null,"abstract":"Ultra wideband (UWB) transmission was evaluated within a small scientific spacecraft, with a view to partly replacing onboard data buses with wireless connections. Spatial distributions of UWB link throughput were derived from measurements. The results revealed that commercially-available UWB devices were capable of accommodating up to around 90-Mb/s data buses within spacecrafts.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"99 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122940158","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}
{"title":"Aircraft wireless sensor network for in-flight fault diagnostics and control","authors":"H. Liu","doi":"10.1109/FBW.2010.5613792","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613792","url":null,"abstract":"Civil aviation has evolved to become a fast and safe transportation over a century's adventure and development. Nevertheless, continuous improvement is sought to make better, greener airplanes, to bring more enjoyable and comfortable experience, and to improve the flight safety and reliability. Aircraft reliability has been one of the primary concerns for aircraft designers, engineers and operators for the past years. One of the technical areas that shows promising feature in improving reliability is the in-flight fault diagnostics and identification (FDI) as well as fault-tolerant control (FTC). Aircraft in-flight faults may result from sensor failures, actuator failures, or even suffers from structural damage. The purpose of FDI is to provide timely accurate fault detection, isolation and confirmation. Moreover, FTC shall enable the aircraft to operate safely with graceful performance degradation.","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"53 12","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"113981563","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}
{"title":"Application of wireless technology to CALVEIN launch vehicles","authors":"John Culbertson, E. Besnard, J. Garvey","doi":"10.1109/FBW.2010.5613789","DOIUrl":"https://doi.org/10.1109/FBW.2010.5613789","url":null,"abstract":"The CALVEIN (California Launch Vehicle Education Initiative) program is a partnership between Garvey Spacecraft Corporation (GSC) and California State University Long Beach (CSULB) whose mission is to provide students the opportunity to build, design, and flight test low cost launch vehicles for education and technology development purposes. Through this work we have received contracts and teamed up with multiple government agencies, organizations and universities to test new aerospace technologies on our low cost launch vehicles. In our position we are able to, and have rapidly tested new wireless aerospace technologies, which we plan to continue in the future as we implement and mature these technologies in the production of our Nano-satellite Launch Vehicle (NLV).","PeriodicalId":219751,"journal":{"name":"CANEUS Fly by Wireless Workshop 2010","volume":"400 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132380909","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}