The Experts below are selected from a list of 246 Experts worldwide ranked by ideXlab platform

Hare Krishna Ratha - One of the best experts on this subject based on the ideXlab platform.

  • High power UHF transmitters using SSPA for Flight Termination System in test range: A detailed study
    2017 IEEE International Conference on Circuits and Systems (ICCS), 2017
    Co-Authors: Romio Rosan Sahani, Utpal Mandal, Anupam Shrivastava, Hare Krishna Ratha
    Abstract:

    This paper discusses on 1KW CW UHF transmitter Systems based on solid state power devices used in Flight Termination System (FTS) in test range. Transmitters based on three different device technologies are studied. These power devices are silicon based bipolar junction transistor (Si-BJT), silicon based double diffused metal oxide transistor (Si-DMOS) and gallium nitride based high electron mobility transistor (GaN HEMT). It aims to present some of our requirement in terms of transmitter's performance in FTS applications. In such application where operating conditions and requirements are very stringent, wideband semiconductor technology is seen as a potential candidate over conventional device technology. A linear and efficient amplifier System is highly required along with good thermal management, broadband operation, reliability and size & weight. System performance parameters like output power, gain, harmonics and IMD are measured for each transmitter and compared. Gallium nitride being a wide band semiconductor and with its HEMT topology provides superior performance in terms of power density, linearity, efficiency and also more reliable.

  • FPGA Implementation of a Tone-Based Flight Termination System in a Software-Defined Radio Platform
    IEEE Transactions on Industrial Informatics, 2017
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper outlines the design and implementation of a tone-based Flight Termination System (FTS) in a software-defined radio (SDR) platform. It is completely a novel implementation of an analog FTS in an SDR platform of NI Flex-RIO System. This single platform based design appears as a substitute for the previously used multiple platforms based complex System. Ruggedization and relevance design methods are required for the FTS design. Hence, the blueprint of the FTS is carried out in a field-programmable gate array. It ensures reconfigurable, interoperable operations with precise, reliable, and future upgradable implementation. Efficient optimization methods have been adopted to minimize the use of hardware resources. LabVIEW, a graphical programming language, is used for rapid prototyping. The validation of the System was done both in subSystem level as well as the integrated level at real-time mission scenario.

  • Implementation of SCADA/HMI System for real-time controlling and performance monitoring of SDR based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • implementation of scada hmi System for real time controlling and performance monitoring of sdr based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • FPGA Implementation of Software Defined Radio-Based Flight Termination System
    IEEE Transactions on Industrial Informatics, 2015
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper proposes a field-programmable gate array (FPGA)-based software defined radio (SDR) implemented Flight Termination System (FTS). This is purely a new kind of implementation of digital FTS in SDR platform. The applied design procedure replaces a multiple platform-based System with a single platform. It also guarantees reconfigurable, interoperable, portable, and handy FTS, and maintains errorless, bug free, and reliable implementation. Real-time Flight Termination operation demands a very highly reliable and ruggedized platform. Hence, the FTS is implemented in FPGA. In order to minimize hardware resources and to enable future upgradation, efficient optimization technique has been applied. LabVIEW, a high-level programming language is used to simulate and implement the System in real time and enables rapid prototyping. The System was validated at subSystems level by measurements of different parameters in various intermediate stages of processing, and further was validated as an integrated System at real-time telecommunication operation environment.

Amiya Ranjan Panda - One of the best experts on this subject based on the ideXlab platform.

  • FPGA Implementation of a Tone-Based Flight Termination System in a Software-Defined Radio Platform
    IEEE Transactions on Industrial Informatics, 2017
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper outlines the design and implementation of a tone-based Flight Termination System (FTS) in a software-defined radio (SDR) platform. It is completely a novel implementation of an analog FTS in an SDR platform of NI Flex-RIO System. This single platform based design appears as a substitute for the previously used multiple platforms based complex System. Ruggedization and relevance design methods are required for the FTS design. Hence, the blueprint of the FTS is carried out in a field-programmable gate array. It ensures reconfigurable, interoperable operations with precise, reliable, and future upgradable implementation. Efficient optimization methods have been adopted to minimize the use of hardware resources. LabVIEW, a graphical programming language, is used for rapid prototyping. The validation of the System was done both in subSystem level as well as the integrated level at real-time mission scenario.

  • Implementation of SCADA/HMI System for real-time controlling and performance monitoring of SDR based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • implementation of scada hmi System for real time controlling and performance monitoring of sdr based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • FPGA Implementation of Software Defined Radio-Based Flight Termination System
    IEEE Transactions on Industrial Informatics, 2015
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper proposes a field-programmable gate array (FPGA)-based software defined radio (SDR) implemented Flight Termination System (FTS). This is purely a new kind of implementation of digital FTS in SDR platform. The applied design procedure replaces a multiple platform-based System with a single platform. It also guarantees reconfigurable, interoperable, portable, and handy FTS, and maintains errorless, bug free, and reliable implementation. Real-time Flight Termination operation demands a very highly reliable and ruggedized platform. Hence, the FTS is implemented in FPGA. In order to minimize hardware resources and to enable future upgradation, efficient optimization technique has been applied. LabVIEW, a high-level programming language is used to simulate and implement the System in real time and enables rapid prototyping. The System was validated at subSystems level by measurements of different parameters in various intermediate stages of processing, and further was validated as an integrated System at real-time telecommunication operation environment.

Debahuti Mishra - One of the best experts on this subject based on the ideXlab platform.

  • FPGA Implementation of a Tone-Based Flight Termination System in a Software-Defined Radio Platform
    IEEE Transactions on Industrial Informatics, 2017
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper outlines the design and implementation of a tone-based Flight Termination System (FTS) in a software-defined radio (SDR) platform. It is completely a novel implementation of an analog FTS in an SDR platform of NI Flex-RIO System. This single platform based design appears as a substitute for the previously used multiple platforms based complex System. Ruggedization and relevance design methods are required for the FTS design. Hence, the blueprint of the FTS is carried out in a field-programmable gate array. It ensures reconfigurable, interoperable operations with precise, reliable, and future upgradable implementation. Efficient optimization methods have been adopted to minimize the use of hardware resources. LabVIEW, a graphical programming language, is used for rapid prototyping. The validation of the System was done both in subSystem level as well as the integrated level at real-time mission scenario.

  • Implementation of SCADA/HMI System for real-time controlling and performance monitoring of SDR based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • implementation of scada hmi System for real time controlling and performance monitoring of sdr based Flight Termination System
    Journal of Industrial Information Integration, 2016
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    Abstract Flight Termination System (FTS) is an important System to control and terminate a wayward Flight vehicle under performance evaluation in test centre. Hence, the functional behavior assessment of the FTS System in real time is of utmost importance in test centre. In this paper, a Supervisory control and data acquisition (SCADA)/human machine interface (HMI) based System with integrated data acquisition (DAQ) facility has been designed, developed and implemented for controlling and monitoring of FTS remotely. The SCADA/HMI based System receives various intermediate processed data from FTS and parameters of onboard command reception System (CRS) from telemetry stations through Ethernet via FTS. It consists of HMI based control and monitoring unit, SCADA server, FTS and validated onboard receiver. All the FTS transmission, reception and onboard reception parameters are monitored and logged in real time, which is used for data analysis. Moreover, the FTS operational setting parameters are controlled by this System remotely. Hence, the developed System is a combination of SCADA/HMI as well as control and monitoring architecture based System implementation. The System architectures involved and the internal implementation of different modules are described here. The performance results are presented and the System is validated in real-time Tele-communication operation environment.

  • FPGA Implementation of Software Defined Radio-Based Flight Termination System
    IEEE Transactions on Industrial Informatics, 2015
    Co-Authors: Amiya Ranjan Panda, Debahuti Mishra, Hare Krishna Ratha
    Abstract:

    This paper proposes a field-programmable gate array (FPGA)-based software defined radio (SDR) implemented Flight Termination System (FTS). This is purely a new kind of implementation of digital FTS in SDR platform. The applied design procedure replaces a multiple platform-based System with a single platform. It also guarantees reconfigurable, interoperable, portable, and handy FTS, and maintains errorless, bug free, and reliable implementation. Real-time Flight Termination operation demands a very highly reliable and ruggedized platform. Hence, the FTS is implemented in FPGA. In order to minimize hardware resources and to enable future upgradation, efficient optimization technique has been applied. LabVIEW, a high-level programming language is used to simulate and implement the System in real time and enables rapid prototyping. The System was validated at subSystems level by measurements of different parameters in various intermediate stages of processing, and further was validated as an integrated System at real-time telecommunication operation environment.

Effendi Dodi Arisandi - One of the best experts on this subject based on the ideXlab platform.

  • sistem pengaman power shape charge pada Flight Termination System power shape charge security System on Flight Termination System
    Jurnal Teknologi Dirgantara, 2017
    Co-Authors: Effendi Dodi Arisandi
    Abstract:

    Battery is reusable electric energy resource. Thus, the battery can be used as power for various kind of electronics equipment. The Fligt Termination System (FTS) module also uses battery as  electric energy resource. The FTS module which has been integrated in the rocket System must be controlled strictly in order to avoid accident that can be caused by switching on the battery power. (Smart System yang menjadi focus pada penelitian ini terdiri dari komponen mikrokontroller, inverter, relay, resistor, dan thyristor-belum ada terjemahan untuk ini). This research was focused on how to protect battery resource as power shape-charge in the FTS module. The research showed that  smart System usage could obstruct the activation of the relay when the battery power is switched on.  Abstrak Baterai adalah sumber energi listrik yang dapat digunakan secara berulang-ulang.  Dengan demikian, baterai dapat digunakan sebagai sumber energi listrik untuk berbagai macam peralatan elektronika. Modul Flight Termination System (FTS ) juga menggunakan baterai sebagai sumber energi listrik. Modul FTS yang telah terintegrasi dalam sistem roket harus dikontrol secara ketat agar tidak terjadi kecelakaan yang dapat ditimbulkan oleh penyalaan power modul. Hal ini disebabkan, pada saat power modul FTS dinyalakan maka akan menimbulkan logika high pada mikrokontroller yang dapat memicu aktifnya komponen elektronika. Penelitian ini fokus pada sistem proteksi sumber daya baterai sebagai pemicu sistem shape-charge pada modul FTS. Smart System yang menjadi fokus pada penelitian ini terdiri dari komponen mikrokontroller, inverter , relay , resistor , dan thyristor . Dari hasil penelitian diperoleh bahwa penggunaan smart System dapat menghambat aktifnya relay yang diakibatkan oleh penyalaan power modul FTS.

  • MULTI FREKUENSI ENCODER Flight Termination System (MULTI FREQUNECY ENCODER Flight Termination System)
    LAPAN, 2015
    Co-Authors: Effendi Dodi Arisandi
    Abstract:

    Flight Termination System (FTS) adalah suatu sistem yang digunakan untuk menghentikansuatu misi peluncuran wahana udara apabila wahana tersebut mengalami kegagalan dalam misinya.Encoder FTS adalah bagian dari FTS yang akan memberikan sinyal perintah dalam bentuk gelombangsinus dengan frekuensi tertentu. Sinyal sinus yang secara umum disebut sinyal tone ranging dapatdibangkitkan dalam rentang frekuensi audio, 20Hz-20KHz. Metode Direct Digital Synthesis (DDS)dapat digunakan untuk membangkitkan sinyal tone ranging yang berupa sinyal sinus atau kotak(pulse). Kerahasiaan sinyal tone ranging yang dikirimkan pada bagian penerima FTS sangat pentingagar tidak bisa diganggu oleh sinyal lain. Dengan menggunakan metode DDS AD9850, dapatdihasilkan sinyal sinus multi frekuensi pada endcoder FTS; 750Hz, 1000Hz, dan 1250Hz.Hal. 87-93: ilus.; 30 cm

  • DESIGN AND DEVELOPMENT OF LOW COST Flight Termination System ENCODER BASED ON DDS AD9850 FOR Flight VEHICLE
    LAPAN, 2015
    Co-Authors: Effendi Dodi Arisandi
    Abstract:

    FTS (Flight Termination System) is a System that used to terminate a mission on the air vehicle such as; rocket, aircraft, and UAV (unmanned air vehicle). FTS is basic safety on the rocket launch for anticipation mission fail. FTS consists 2 Systems; encoder System (in transmitter System) and decoder System (in the receiver System). This research just focused on the FTS encoder with generates the sine waveform as signal tone. The method transmitted FTS signal by using radio transceiver HT (handy-talky) with frequency VHF and the audio frequency as the FTS signal tone. The encoder System can generate the audio frequency from 20 Hz till 20 KHz as sine waveform by use DDS method. The experiment results shown that the DDS AD9850 can generate the sine waveform from 0 Hz till 40 MHz depend on the frequency given.p. 52-5

Tracy Woodard - One of the best experts on this subject based on the ideXlab platform.

  • Development of a Subminiature Enhanced Flight Termination Receiver
    2011
    Co-Authors: Tracy Woodard, Jeff Vetter, Jason Rodzinak
    Abstract:

    As the size of missiles and UAVs shrink, so does the volume available for the Flight Termination System (FTS). Small, light weight FTS Systems open up applications not possible with the larger and heavier conventional FTS Systems. This paper presents a novel approach for the design, implementation and test of a subminiature Flight Terminate System Receiver for use in the Subminiature Flight Safety System (SFSS). This receiver implements the new digital-based Enhanced Flight Termination System (EFTS) protocol, while maintaining a volume of less than 1 cubic inch with power consumption of less than 2 watts. Combining all of the necessary functionality into a small package while meeting the rigorous requirements of the Range Commanders Council (RCC) specifications (EMI, vibration and shock) presented significant challenges. The Subminiature Enhanced Flight Termination Receiver used in the SFSS has been named the “SEFTR”.

  • The Subminiature Flight Safety System
    2011
    Co-Authors: Tracy Woodard, Chris Dehmelt
    Abstract:

    Weapons platform testing and monitoring have historically consisted of custom telemetry and Flight safety System solutions tailored to the requirements (including Title 10 Mandates) and size constraints of individual platforms. The size of these individual components of these Systems has necessitated that warhead replacement to facilitate insertion of these units to support test and evaluation activities. Currently there are no products available to meet these requirements in a miniaturized and modular package. L-3 Communications Telemetry East (L-3 TE) has developed an extensive background in providing solutions to gather vital missile and target information over the last several decades. Under the auspices of Eglin AFB, L-3TE is leading a multi-disciplinary team to design and develop the Subminiature Flight Safety System (SFSS) to support existing and new weapons applications. SFSS is a universal, small, and low cost redundant Flight Termination System (FTS) that incorporates encoding, processing and TSPI capacities that provides critical health/safety/welfare monitoring and allows for highly efficient telemetering of all weapon application and FTS data. The SFSS is intended as a solution to allow weapon System developers, test agencies, and range safety officers the ability to track, monitor, and if necessary, terminate all types of weapon Systems. It is designed to interface with newly developed weapon Systems, while providing backward compatibility to meet existing requirements with minimal modifications to the weapon. The SFSS components are intended to significantly reduce the cost and improve the quality of test support by providing a highly integrated solution that minimizes physical intrusion into weapon Systems, by eliminating the need for warhead removal. In addition, a common hardware platform will reduce overall System cost of acquisition and maintenance to the government, a key element in today’s world of stressed budgets.