Design and fabrication of advance level CANSAT Used for measuring the atmospheric parameters And GPS tracking system (original) (raw)

Design Review of Satellite Telemetry based on CCSDS standards and Proposed Hardware Implementation of CanSat

… of the International MultiConference of Engineers …, 2008

Satellite Communication is one of the most impressive spin-offs from the space programmes and has made a major contribution to, indeed totally altered, the patterns of International communication. Communication by satellite evolved from the simple technology of "Early Bird" to the highly sophisticated present-day satellites" [1]. The potential of the outer space as a communication hub is great and at the heart of this is the satellite. This paper aims at developing a micro-satellite, which can be used for educational purposes as well as a stepping stone for further complex developments. Data from this satellite will be formatted on the basis of the CCSDS (Consultative Committee for Space Data Systems) standards before transmission. We will also highlight one of the simplest designs of the micro satellite CanSat (Satellite in a can) at university level with most cheaply and easily available resources ever highlighted for the Space Education in Asia.

Experimental Approach for the Evaluation of the Performance of a Satellite Module in the CanSat Form Factor for In Situ Monitoring and Remote Sensing Applications

International Journal of Aerospace Engineering, 2021

This article includes the phases of conceptualization and validation of a picosatellite prototype named Simple-2 for remote sensing activities using COTS (Commercial-Off-The-Shelf) components and the modular design methodology. To evaluate its performance and ensure the precision and accuracy of the measurements made by the satellite prototype, a methodology was designed and implemented for the characterization and qualification of CanSats (soda can satellites) through statistical tests and techniques of DoE (Design of Experiments) based on CubeSat aerospace standards and regulations, in the absence of official test procedures for these kinds of satellite form factor. For the above, two experimental units were used, and all the performance variables of the different satellite subsystems were discriminated. For the above, two experimental units were used, and all the performance variables of the different satellite subsystems were discriminated against. These were grouped according t...

A pico-satellite assembled and tested during the 6th CanSat Leader Training Program

In this paper, we describe the process to construct a pico-satellite mounted in a bottle of polyethylene terephthalate (PET) of 345 ml. The assembly and tests were made during the 6th CanSat Leader Training Program (CLTP-6) at University Hokkaido-Japan in the summer 2015. The pico-satellite was launched in the facilities of Uematsu Electric Co. Ltd. in Akabira-Japan by a paper model rocket, which achieved a height of approximately 100 m. The mission was designed to measure physical variables, such as temperature and humidity using electronic sensors. During the flight, we observed that the temperature inside the rocket was ∼0.5 • C higher than the temperature of the environment. We registered a humidity difference of ∼5%, measured between the maximum height and the landing point. The flight pattern was projected to a plane that covers an area of 50 m × 50 m by means the coordinates of a GPS.

Model Satellite Design for CanSat Competition

— Objective of this work is to design and manufacture a model satellite named Vecihi that is able to perform some of the basic tasks that artificial satellites perform. The satellite is developed under the rules of CanSat Competition 2013, which aims to promote innovative space solutions and to improve the current systems. The Vecihi satellite designed around budgetary, dimensional, and mass requirements as set in the competition guidelines, while carrying and landing its payload successfully.

Approaching a nano-satellite using CAN-SAT systems

—Conquest of the space spreads with small educational projects that aim to explore the capabilities and the potentials that the mankind have. This paper concludes our experiments that led to launching the second Can-Sat form Alexandria, Egypt under affiliation of Space and Technology Program in Bibliotecha Alexandrina. Here we presents our satellite system and the communication system that connects the ground station to the flying system, as well it represents the launching procedure, and some of the problems we overboard during our project duration

GROUND STATION DESIGN PROCEDURES FOR CANSAT

CANSAT's are getting more popular each day in aerospace engineering curriculums because they enable the students to have hands-on experience on virtual satellite launch operations. This paper presents design and implementation of a PC based ground station for CANSAT's. So far, most of the emphasis has been built on the hardware and software inside the CANSAT. However, during the competitions it has been observed that even though the CANSAT works perfectly, the ground station frequently fails therefore leading to mission failure. In this study a ground station is developed from scratch using a high level language (C#) and the procedure is defined briefly. The station is platform-free therefore it may operate with any CANSAT having different brand microcontrollers. The users may track several parameters and send control commands simultaneously. The ground-station is one of the most important aspects of CANSAT trials however, for the beginners it may be challenging to provide all these features at once. This study defines many practical aspects of designing ground stations so that more emphasis may be given to the design of CANSAT hardware and software.

A Conceptual Design Synthesis for the Model Satellite

Journal of Aeronautics and Space Technologies, 2020

The annually organised Türksat Satellite Model Competition gives undergraduate and graduate students, the opportunity to transform theoretical knowledge into practice and to share interdisciplinary work and experience. Bulent Ecevit University participated in the Türksat Satellite Model Competition 2019 with B-Dispate Black Diamond Space Team. The team consists of undergraduate students with different engineering backgrounds, who are supervised by the academic as well as industry advisors. The main goal of the team is to send the telemetry information (pressure, height, battery state of charge, photograph and video recording, equipment opening, landing location information, attitude information, etc.) collected by the sensor equipments on board to the ground station during the flight stage. Also, the team will have to fulfil particular tasks specified by the competition board. A comprehensive conceptual model satellite synthesis is reported in this paper. The steps in designing the model satellite are presented, allowing significant savings in terms of qualification tests and giving way to a procedure to design and manufacture a low-cost educational microsatellite.

DESIGN OF A GENERIC PLATFORM FOR AN EDUCATIONAL CANSAT

Satellites play a major role in nowadays world. Engineering schools face the challenge of preparing engineers for the needs of such industry, with multidisciplinary capabilities. In Brazilian reality, Astronautical Engineering still needs investments and development for undergraduate courses. Some tools can help in this context, as CanSats and CubeSats. CanSats are a suitable way to provide the students with a hands on tool, being cheaper and simpler than a CubeSat, but having all main subsystems of a conventional satellite. Principles of Systems Engineering, design of aerospace devices and fundamental techniques can be learnt. Students design every subsystem of the device, test, integrate and operate them, taking part of their whole lifecycle. As a demand for this educational tool, a detailed study of its structure and the design of a generic adaptable platform was performed. The objective was to design a generic platform for a CanSat easily adaptable for different missions. It is assumed the device will fly attached to a balloon. Results include the simulations and two 3D designs ready to be built, using resources usually available for engineering schools. For cases when the present model is not suitable, the paper presents a methodology for analysing different cases.

Design, Implementation, and Operation of a Small Satellite Mission to Explore the Space Weather Effects in Leo

Aerospace

Ten-Koh is a 23.5 kg, low-cost satellite developed to conduct space environment effects research in low-Earth orbit (LEO). Ten-Koh was developed primarily by students of the Kyushu Institute of Technology (Kyutech) and launched on 29 October 2018 on-board HII-A rocket F40, as a piggyback payload of JAXA’s Greenhouse gas Observing Satellite (GOSAT-2). The satellite carries a double Langmuir probe, CMOS-based particle detectors and a Liulin spectrometer as main payloads. This paper reviews the design of the mission, specifies the exact hardware used, and outlines the implementation and operation phases of the project. This work is intended as a reference that other aspiring satellite developers may use to increase their chances of success. Such a reference is expected to be particularly useful to other university teams, which will likely face the same challenges as the Ten-Koh team at Kyutech. Various on-orbit failures of the satellite are also discussed here in order to help avoid th...