Techavijit, Pirada

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Techavijit, Pirada
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pirada.te@kmitl.ac.th

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Now showing 1 - 7 of 7
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    CubeSat image transmission in JPEG compression: An experiment on high altitude platform
    (2016-03-23)
    Techavijit, Pirada
    ;
    Chivapreecha, Sorawat
    ;
    Sukchalerm, Polkit
    ;
    Plodpai, Aniwat
    CubeSat is a type of picosatellite which is developed with the purposes of promoting and development the skills necessary for the design, manufacturing, and testing of small satellites in the future. This paper presents our work on CubeSat design and development which focuses on JPEG compression and transmission to ground station. And this paper also uses the high altitude balloon to verify CubeSat functions as it is low cost experiments but can provide conditions similar to spacelike: pressure, temperature, air density as well as distance for communication. This paper will discuss the testing result of CubeSat on high altitude balloon to examine functions, verify link budget and signal strength in stratosphere at maximum altitude of 24 kilometers.
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    Power Requirements for Battery Maintenance and Temperature Profile on High Altitude Platform
    (2024-01-01)
    Techavijit, Pirada
    ;
    Sukchalerm, Polkit
    ;
    Wongphuangfuthaworn, Natthapong
    ;
    Iamsawat, Jakkrit
    Experiments on high-altitude platform (HAP) at the nearspace must be faced with extremely low temperatures, reaching as low as -50 degrees Celsius, which exceeds the operational range of electronic systems. Especially, the battery that requires a heating system and thermal insulation. This paper will report temperature profile on the HAP flight and the results of experiments with the installation of the heating system to determine its adequacy, and measuring the electrical power needed for heating.
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    Simplified Design and Development of Radio-Tracking on Thai-Traditional Rocket (Bang Fai) With Real Case Experiments
    (2023-01-01)
    Techavijit, Pirada
    ;
    Sukchalerm, Polkit
    Thousands of large-scale homemade rockets (Bang Fai) are fired during Thai rocket festival annually. To prevent harm to airspace and ground, this paper proposes the design and development of a radio-tracking system that can report the velocity and altitude in real-time. The design is simplified with its small size and inexpensive price but still works with the rocket's dynamics. This paper also reports the results of rockets' ascent/descent velocities and their altitudes from tracking system mounted on the rockets. All this data can be used for evaluating the airspace and ground risks and for improving the design for future developments.
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    Potential of Photovoltaic on Small Stratospheric Satellite in Real-World Experiment
    (2023-01-01)
    Techavijit, Pirada
    ;
    Wongphuangfuthaworn, Natthapong
    ;
    Sukchalerm, Polkit
    ;
    Plodpai, Aniwat
    This paper investigates the potential of monocrystalline photovoltaic (PV) panels to generate power when installed on stratospheric satellites through near-space flight experiments conducted at altitudes of 0-23 kilometers above sea level. It also compares the results with a mathematical model developed by ASHRAE in previous research, which reveals the differences caused by various factors such as atmospheric attenuation and high-level clouds. The main objective of this study is to identify the optimal altitude for deploying stratospheric satellites with appropriately sized PV panels that can generate sufficient power to meet the communication system's requirements for long-term operation.
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    Suitable altitude for long-operated communication high altitude balloon with experimental flights
    (2016-03-23)
    Techavijit, Pirada
    ;
    Chivapreecha, Sorawat
    ;
    Sukchalerm, Polkit
    ;
    Wongphuangfuthaworn, Natthapong
    High Altitude Platform (HAP) is a platform for many purposes e.g. remote sensing, communication, science experiment etc. Several countries are likely interested in research and development of HAP for communication since it combines the benefits of terrestrial and satellite systems. The objective of this paper is to find the suitable altitude to operate zero-pressure balloons, a type of high altitude platform which maintainable of desired altitude, for longest duration. This paper presents an experiment of zero-pressure balloon including design and development. The main parameters considered in this study are wind data and RF propagation. The wind data has been collected from several sources: from daily weather balloons recorded for 5 years and from the experimental balloon flights. This paper will discuss the suitable altitude for operating the zero-pressure balloons for longest duration without any control system. This paper shall also recommend altitude for further study.
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    Communication Link Margin Design for Picosatellite operating on HAP
    (2024-01-01)
    Techavijit, Pirada
    ;
    Sukchalerm, Polkit
    This paper examines the testing of Picosatellites on Highaltitude Platforms (HAPs), conducting experiments to collect data at stratosphere or near-space. This involves long-distance over hundreds of kilometers telecommunication between ground stations and HAP. This paper will suggest designing an appropriate link margin from ground to Picosatellites on HAPs, by utilizing data from actual experiments for analysis and presentation.
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    Under ∃300 Anti-drone gun with GPS spoofing technique using COTS
    (2024-01-01)
    Techavijit, Pirada
    ;
    Sukchalerm, Polkit
    ;
    Pitchsanupun, Montawat
    ;
    Kijatanath, Natcha
    This research presents the development of a cost-effective anti-drone gun. The system utilizes Commercial Off-The-Shelf (COTS) components for scalability and rapid development. The system employs GPS spoofing using Software-Defined Radio (SDR) devices, offering a straightforward and energyefficient solution compared to other complex anti-drone techniques. The prototype successfully manipulates coordinates, tricking commercial drones into autonomously landing in designated zones, showcasing a practical and resource-efficient approach to drone deterrence.