BEGIN:VCALENDAR VERSION:2.0 PRODID:IEEE vTools.Events//EN CALSCALE:GREGORIAN BEGIN:VTIMEZONE TZID:Asia/Kolkata BEGIN:STANDARD DTSTART:19451014T230000 TZOFFSETFROM:+0630 TZOFFSETTO:+0530 TZNAME:IST END:STANDARD END:VTIMEZONE BEGIN:VEVENT DTSTAMP:20240710T075629Z UID:356EA3B2-4CFA-4C44-88DE-7DC85A65B3B1 DTSTART;TZID=Asia/Kolkata:20240629T094500 DTEND;TZID=Asia/Kolkata:20240629T132000 DESCRIPTION:[]\n\nThis is the Inaugural Event of IEEE Sensors Council Chapt er\, Methodist College of Engineering and Technology Student Branch. This event was planned to inaugurate the newly formed Sensors Council Chapter i n the Student Branch followed by a talk on Application of Sensors in Missi le and Launch Vehicles: Future Trends by Dr. Joydeb Chattopadhyay.\n\nAbst ract of the talk:\n\nSensor converts physical event to the information tha t is processed and analyzed by the computing system for a specific purpose . Sensors are used in all application like agriculture\, medical\, transpo rtation\, aerospace technologies and many others. In this talk role of sen sors will be discussed in the area of Missile and Launch Vehicle. These tw o systems have many similarities in operation. Missiles are required to hi t the target located at long distance and Launch vehicles are required to launch a satellite to the particular orbit. They both have multiple stages and follow a similar trajectory in the boost phase. They use large number of sensors in different form. These sensors can be broadly categorized in two roles like a) Guidance\, control and navigation b) Telemetry operatio n.\n\nThe vehicle is provided initial coordinates of the launch point and also the destination point. The computer embedded in these vehicles receiv es sensor data and execute Navigation and guidance algorithm and control t he flight path through set of actuation system. Gyros and accelerometers a re the basic sensors used for this purpose. In addition\, there are other sensors like current sensors and LVDTs used for actuation sensors. To achi eve best hit seekers are used in different frequency band. Flight vehicle has many subsystems like structure\, propulsion\, aerodynamics\, avionics\ , power sources. These system performances are assessed by the measurement of difference parameters like temperature\, pressure\, strain\, acoustic\ , vibration\, current\, voltage etc. They are captured through the sensors suitably attached to the particular system. These are acquired and by dat a acquisition system and transferred to telemetry system with pulse code m odulator and transmitter. The transmitted signal is received at the ground station for necessary analysis and decision making. These sensors are dis cussed in details and also shortcomings of the sensor interfacing the data acquisition system and to the telemetry is brought out. A CAN bus-based a rchitecture with intelligent sensors is brought out as future work.\n\nCo- sponsored by: Methodist College of Engineering and Technology\n\nSpeaker(s ): Dr. Chattopadhyay\n\nBldg: D-Block\, Seminar Hall\, 4-1-1061/A\, Method ist College of Engineering and Technology\, Boggulakunta\, Abids.\, Hydera bad\, Andhra Pradesh\, India\, 500001 LOCATION:Bldg: D-Block\, Seminar Hall\, 4-1-1061/A\, Methodist College of E ngineering and Technology\, Boggulakunta\, Abids.\, Hyderabad\, Andhra Pra desh\, India\, 500001 ORGANIZER:ieeesb_mcet@methodist.edu.in SEQUENCE:10 SUMMARY:A Technical Talk on "Application of Sensors in Missile and Launch V ehicles: Future Trends" URL;VALUE=URI:https://events.vtools.ieee.org/m/427044 X-ALT-DESC:Description: <br /><p style="text-align: justify\;">&nbsp\;</p>\ n<p style="text-align: justify\;"><img src="https://events.vtools.ieee.org /vtools_ui/media/display/ebcc9584-d825-4cc6-a8bd-61173df5d7e8" alt="" widt h="800" height="400"></p>\n<p style="text-align: justify\;">&nbsp\;</p>\n< p style="text-align: justify\;">This is the Inaugural Event of IEEE Sensor s Council Chapter\, Methodist College of Engineering and Technology Studen t Branch.&nbsp\; This event was planned to inaugurate the newly formed Sen sors Council Chapter in the Student Branch followed by a talk on Applicati on of Sensors in Missile and Launch Vehicles: Future Trends by Dr. Joydeb Chattopadhyay.</p>\n<p style="text-align: justify\;">&nbsp\;</p>\n<p style ="text-align: justify\;">Abstract of the talk:</p>\n<p style="text-align: justify\;">Sensor converts physical event to the information that is proce ssed and analyzed by the computing system for a specific purpose. Sensors are used in all application like agriculture\, medical\, transportation\, aerospace technologies and many others. In this talk role of sensors will be discussed in the area of Missile and Launch Vehicle. These two systems have many similarities in operation. Missiles are required to hit the targ et located at long distance and Launch vehicles are required to launch a s atellite to the particular orbit. They both have multiple stages and follo w a similar trajectory in the boost phase. They use large number of sensor s in different form. These sensors can be broadly categorized in two roles like a) Guidance\, control and navigation b) Telemetry operation.</p>\n<p style="text-align: justify\;">The vehicle is provided initial coordinates of the launch point and also the destination point. The computer embedded in these vehicles receives sensor data and execute Navigation and guidanc e algorithm and control the flight path through set of actuation system. G yros and accelerometers are the basic sensors used for this purpose. In ad dition\, there are other sensors like current sensors and LVDTs used for a ctuation sensors. To achieve best hit seekers are used in different freque ncy band. Flight vehicle has many subsystems like structure\, propulsion\, aerodynamics\, avionics\, power sources. These system performances are as sessed by the measurement of difference parameters like temperature\, pres sure\, strain\, acoustic\, vibration\, current\, voltage etc. They are cap tured through the sensors suitably attached to the particular system. Thes e are acquired and by data acquisition system and transferred to telemetry system with pulse code modulator and transmitter. The transmitted signal is received at the ground station for necessary analysis and decision maki ng. These sensors are discussed in details and also shortcomings of the se nsor interfacing the data acquisition system and to the telemetry is broug ht out. A CAN bus-based architecture with intelligent sensors is brought o ut as future work.&nbsp\;</p> END:VEVENT END:VCALENDAR