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Titlebook: Advances in Small Satellite Technologies; Proceedings of Natio R.S. Priyadarsini,T. Sundararajan Conference proceedings 2023 The Editor(s)

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樓主: Corrugate
41#
發(fā)表于 2025-3-28 16:42:55 | 只看該作者
Sanket—Technology Demonstration of Antenna Deployment System on PSLV Stage 4 Orbital Platformt mission is a technology demonstration designed to be flown on the Indian Space Research Organization’s PSLV Stage 4 Orbital Platform (PS4-OP) (Announcement of opportunity for orbital platform. Indian Space Research Organisation, Bangalore [.]) and aims to qualify the team’s Antenna Deployment Syst
42#
發(fā)表于 2025-3-28 22:34:48 | 只看該作者
Development of a PS4-OP Payload for Technology Demonstration of Small-Satellite Subsystems and technology demonstrations, a unique opportunity has been created to develop and test small-satellite subsystems and instruments as PS4-OP (PSLV 4th Stage Orbital Platform) payloads, prior to the launch of the small satellite itself. The PiLOT (PS4 in-orbital OBC and TTC) payload has been develo
43#
發(fā)表于 2025-3-29 02:35:00 | 只看該作者
Design and Performance Validation of CETSAT Sensor Module Fabricated Using COTS for Low Earth Orbit performed in connection with the student satellite programme of College of Engineering Trivandrum (CETSAT). Various initiatives to democratize space missions have been implemented all over the world. Indeed, COTS components are finding their way into small satellites lately as they lead to significa
44#
發(fā)表于 2025-3-29 05:01:05 | 只看該作者
Design and Development of Cold Gas Propulsion System for Smart Space Robot astronaut exploration activities and also undertake robotic precursor missions. Towards this, design and development of a flying Smart Space Robot (SSR) is initiated. The Smart Space Robot (SSR) is a space flying robot which will be tethered to the unmanned orbital platform on the fourth stage (PS4
45#
發(fā)表于 2025-3-29 07:50:33 | 只看該作者
46#
發(fā)表于 2025-3-29 14:29:50 | 只看該作者
Field-Oriented Control for Performance Improvement in Reaction Wheels and Implementation of Algorithpple in reaction torque will affect the performance of critical on-board instruments such as atomic clock, high-resolution cameras, etc. in the spacecraft. The three-axis stabilization system using reaction wheels aims to provide high-pointing accuracy, low jitter and long-term attitude stability. T
47#
發(fā)表于 2025-3-29 16:53:51 | 只看該作者
Structural Analyses for a Typical Small Satelliteevelopment of small satellites. This enabled many commercial companies to venture in to this area since the development can be made possible with small budget. The market size of small satellite is expected to flourish in the next few years. Small satellites are used mainly in the areas of Earth obs
48#
發(fā)表于 2025-3-29 20:26:24 | 只看該作者
49#
發(fā)表于 2025-3-30 02:24:27 | 只看該作者
S. Q. Wang,R. B. Wilcockson,J. Mannone of the electronic packages designed for Indian communication satellite to meet such vibration loads and methods used to analyze the package virtually (through analysis software) before testing which saves the time and cost by reducing the number of prototypes. Three analyses (Eigen value analysi
50#
發(fā)表于 2025-3-30 06:59:55 | 只看該作者
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