標(biāo)題: Titlebook: Advances in Small Satellite Technologies; Proceedings of Natio R.S. Priyadarsini,T. Sundararajan Conference proceedings 2023 The Editor(s) [打印本頁(yè)] 作者: Corrugate 時(shí)間: 2025-3-21 17:24
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書(shū)目名稱(chēng)Advances in Small Satellite Technologies讀者反饋
書(shū)目名稱(chēng)Advances in Small Satellite Technologies讀者反饋學(xué)科排名
作者: 颶風(fēng) 時(shí)間: 2025-3-21 21:42
PS4-Orbital Platform: An Ideal Suite for Scientific Experiments, data management and specific experimental requirements. In short, ISRO is extending its expertise in space technology to the scientific community as a platform to design, develop and validate their experiments in an effective manner.作者: 粗魯性質(zhì) 時(shí)間: 2025-3-22 01:32
Introduction to near net-shape operations,odel predicts bounding boxes and corresponding class probabilities directly from images in a single assessment. This will result in a real-time object detection of images without compromising accuracy.作者: GRUEL 時(shí)間: 2025-3-22 07:30 作者: GOAD 時(shí)間: 2025-3-22 11:09 作者: 預(yù)測(cè) 時(shí)間: 2025-3-22 15:39
Sanket—Technology Demonstration of Antenna Deployment System on PSLV Stage 4 Orbital Platformnket will be mounted on PS4-OP which remains in LEO for around 6?months. Our Antenna Deployment System is developed as an independent module that is compatible with standard CubeSat sizes 1U, 2U and 3U.作者: Bureaucracy 時(shí)間: 2025-3-22 20:33 作者: 我不死扛 時(shí)間: 2025-3-23 00:39
Testing and Qualification of RF MEMS Switch Demonstrator Payload (RFMEMS-TD1) for Small Satellite Plm?×?110?mm, height 100?mm and power consumption 4.2?W. Telemetry requirements are suitable for typical small satellite missions. The electronics components used are commercial grade which have undergone payload level qualification tests for the intended mission using the proto flight model test philosophy.作者: 透明 時(shí)間: 2025-3-23 05:19
2195-4356 nd engineering, ranging from the control, mechanical, and thermal systems to the sensors, antennas, and RF systems used. The book is of interest to scientists and engineers working on or utilizing satellite and space technologies..978-981-19-7473-1978-981-19-7474-8Series ISSN 2195-4356 Series E-ISSN 2195-4364 作者: 厭倦嗎你 時(shí)間: 2025-3-23 08:32
E. Heinzle,T. Kaufmann,M. Griotaper explores the proliferation of the status of the University/College supported student-built space missions over the last years and the various levels of applications of small satellite platforms in India. Moreover, how the student satellite projects translated into useful small satellite commercial missions is also discussed.作者: CYN 時(shí)間: 2025-3-23 12:46
Introduction to near net-shape operations,, data management and specific experimental requirements. In short, ISRO is extending its expertise in space technology to the scientific community as a platform to design, develop and validate their experiments in an effective manner.作者: Lucubrate 時(shí)間: 2025-3-23 16:55
Conference proceedings 2023lating to small satellite technology. The papers cover various issues relating to design and engineering, ranging from the control, mechanical, and thermal systems to the sensors, antennas, and RF systems used. The book is of interest to scientists and engineers working on or utilizing satellite and作者: NAUT 時(shí)間: 2025-3-23 20:26
2195-4356 al services.Describes utilization of small satellites for co.This book contains select papers presented during the 2nd National Conference on Small Satellites, discussing the latest research and developments relating to small satellite technology. The papers cover various issues relating to design a作者: Mettle 時(shí)間: 2025-3-23 23:50
Seonggeon Bae,Hyungwoo Park,Myungjin Bae-part of the institute’s proposed payload under ISRO’s PS4OP programme. It is being developed as per PocketQube standard with 2P (50?×?50?×?114?mm.,?≤?500?g) unit specifications for satisfying mechanical, power and tracking requirements. The major goals of the satellite include the demonstration of 作者: 盟軍 時(shí)間: 2025-3-24 04:35 作者: BOON 時(shí)間: 2025-3-24 09:53
E. Heinzle,T. Kaufmann,M. Griotal intrinsic worth is the cross-disciplinary training for students that endow a future career in the space industry. The experience in learning and working with hands-on, project-based education proves effective for talent management among the student community. Programs such as the CubeSat standard作者: Ankylo- 時(shí)間: 2025-3-24 11:04
S. Q. Wang,R. B. Wilcockson,J. Mannnerated by the launch vehicle. These electronic packages also known as modules, systems and/or subsystems will experience these vibration loads when mounted in the satellite and must be designed and qualified to meet these launch loads. These modules house the Printed Circuit Board (PCB) on which cr作者: 裝勇敢地做 時(shí)間: 2025-3-24 18:00
Structured Modelling of Bioreactor Systemsall detail of a highly optimized Ku-band Transmit–Receive module consisting of exciter and receiver sub-systems. The exciter receives the IF signal with necessary modulation like Linear Frequency Modulation (LFM) from signal processor module. The IF signal is upconverted to the transmit frequency us作者: 令人不快 時(shí)間: 2025-3-24 22:54
Introduction to near net-shape operations,ys a vital role in a wide range of applications and is receiving significant attention in recent years. Even though many great progress has been made in this field, the detection of multi-scale objects, especially small objects in high-resolution satellite (HRS) and drone images, has not been adequa作者: 慢跑 時(shí)間: 2025-3-24 23:20
Introduction to near net-shape operations, a three-axis-stabilized platform for small scientific payloads to carry out in-orbit scientific experiments for an extended duration of 4–6?months. The PS4 stage has standard interfaces and packages for power generation, telemetry, tele-command, stabilization, orbit keeping and orbit maneuvering. T作者: Trigger-Point 時(shí)間: 2025-3-25 06:11 作者: 不整齊 時(shí)間: 2025-3-25 09:51 作者: 波動(dòng) 時(shí)間: 2025-3-25 12:31
https://doi.org/10.1007/978-0-387-34879-7performed 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作者: forbid 時(shí)間: 2025-3-25 19:52 作者: Liberate 時(shí)間: 2025-3-25 21:44 作者: 我不怕?tīng)奚?nbsp; 時(shí)間: 2025-3-26 00:28
D. A. Adams,C. Irgens,E. MacArthur,B. Leespple 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作者: 鄙視讀作 時(shí)間: 2025-3-26 05:53
High-spatial-resolution remote sensingevelopment 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作者: Lipohypertrophy 時(shí)間: 2025-3-26 09:03 作者: cogent 時(shí)間: 2025-3-26 15:52 作者: Stagger 時(shí)間: 2025-3-26 18:56 作者: 陰謀小團(tuán)體 時(shí)間: 2025-3-26 22:02
Advances in Small Satellite Technologies978-981-19-7474-8Series ISSN 2195-4356 Series E-ISSN 2195-4364 作者: 圖表證明 時(shí)間: 2025-3-27 04:40
R.S. Priyadarsini,T. SundararajanDiscusses design and development of cost-effective satellite systems.Presents applications for scientific, operational, public, and commercial services.Describes utilization of small satellites for co作者: 愛(ài)了嗎 時(shí)間: 2025-3-27 07:01 作者: 孤獨(dú)無(wú)助 時(shí)間: 2025-3-27 10:35 作者: 保留 時(shí)間: 2025-3-27 16:13 作者: Immunotherapy 時(shí)間: 2025-3-27 17:55
Student Small Satellite Design and Development in India: A Reviewal intrinsic worth is the cross-disciplinary training for students that endow a future career in the space industry. The experience in learning and working with hands-on, project-based education proves effective for talent management among the student community. Programs such as the CubeSat standard作者: miscreant 時(shí)間: 2025-3-28 00:50
Analysis and Testing of Space Electronics’ Package to Meet Launch Vehicle Vibration Loadsnerated by the launch vehicle. These electronic packages also known as modules, systems and/or subsystems will experience these vibration loads when mounted in the satellite and must be designed and qualified to meet these launch loads. These modules house the Printed Circuit Board (PCB) on which cr作者: parallelism 時(shí)間: 2025-3-28 04:15 作者: 尊重 時(shí)間: 2025-3-28 07:02 作者: ALIEN 時(shí)間: 2025-3-28 11:40 作者: sterilization 時(shí)間: 2025-3-28 16:42
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作者: ticlopidine 時(shí)間: 2025-3-28 22:34
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作者: 歡呼 時(shí)間: 2025-3-29 02:35
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作者: 不公開(kāi) 時(shí)間: 2025-3-29 05:01
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作者: ECG769 時(shí)間: 2025-3-29 07:50 作者: 輪流 時(shí)間: 2025-3-29 14:29
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作者: Arresting 時(shí)間: 2025-3-29 16:53
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作者: 釋放 時(shí)間: 2025-3-29 20:26 作者: 情愛(ài) 時(shí)間: 2025-3-30 02:24
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作者: Neonatal 時(shí)間: 2025-3-30 06:59 作者: 陳腐的人 時(shí)間: 2025-3-30 09:35 作者: Predigest 時(shí)間: 2025-3-30 15:08 作者: 說(shuō)笑 時(shí)間: 2025-3-30 20:14 作者: Anguish 時(shí)間: 2025-3-30 22:56
Xiujuan Feng,Jie Gao,Rongxi Tangl mode of the laser including path length control signal, high frequency oscillator signal and dithering frequency variations. We applied these data on linear and polynomial regression models and obtained up to 76% and 88% reduction in bias drift, respectively. Further, the denoising filter is studi作者: dissent 時(shí)間: 2025-3-31 01:52
