Infinite Orbits’ Post

The new year of 2024 brings us new possibilities, ambitions, and ways to achieve them. OKB Fifth Generation proudly presents its latest development - the TriSAT picosatellite. This technology aims to replicate the functionality of a basic CubeSat mission and make space programs more accessible to universities and institutions. TriSAT is a single-board picosatellite, weighing up to 0.5 kg. In its transport position, it folds into a triangular prism. In working position, it unfolds into a plane. The TriSAT deployer for four such units complies with 1U of the CubeSat standard. TriSAT is well suited for educational missions and for taking the first step towards space exploration. In particular, such project as a picosatellite mission will serve as an excellent diploma project for student groups and will provide great experience and qualifications for a future career in aerospace engineering. Moreover, the presence of the Raspberry Pi Zero allows for a variety of experiments in orbit. As a client-oriented and technologically advanced company, OKB5 can provide the full spectrum of space-mission related services or an individual solution tailored to your specific needs. Some of these solutions include crucial steps for any space mission, such as: — training activities and educational programs in aerospace; building a TriSAT satellite mission that meets your needs or one based on our in-house standards; — testing services, payload adaptation, and integration; — launch services; — telemetry, tracking, and command services using the in-house GRID software and the network of GRID ground stations. And the main news is that this year, 8 picosatellites will be launched into orbit and are already available for booking for your tasks! Contact us, and we will be happy to tell you more: https://lnkd.in/e6wmR95g

Delighted to share my significant role in designing the external structure, assisting in movement using the rocker-bogie system, and developing the actuator linear arms for the Mars Rover Prototype project  This collective effort led by EgSA-Egyptian Space Agency and NSST_BSU the mysteries of the Red Planet! 🚀 🚀 Exciting News from the World of Space Exploration! 🌌 🔭 Designing and developing a Mars Rover Prototype 🤖 Join me in learning journey exploring the fascinating world of Mars exploration and the development of a Mars Rover Prototype! 🛰️ 🌟 Key Highlights: 🔍 Objectives: Designing a Mars rover for detailed scientific research, addressing Martian environment challenges, and ensuring mission success. 🌍 Environment Conditions: From extreme temperatures to low gravity, the Martian environment presents unique challenges. 🛠 Structure: Overview, design, and simulation of the rover's mechanism, manufacturing, and actuator linear arm. 📡 Communication: Data transmission via direct links to Earth and through orbiters using antennas. ☀️ Power System: Critical for rover operation, utilizing solar panels, lithium-ion batteries, and a radioisotope thermoelectric generator. 🔬 Payload: Equipped with instruments like Soil Analysis Tools Sensors, cameras, Weather Station Sensors:, and communication equipment . Let's dive into the intricacies of creating a vehicle to explore the Red Planet and unravel its mysteries! 🚀 supervisor by: Dr. Mohamed Elfarran,PhD Assistant Professor at NSST Eng. Ahmed Yahia Embedded Software Engineer at EgSA Team member: Mostafa Gaber Samar Mohamed Amira Meshref shimaa alktib Mohammed Yosri Mohamed Helmy Youssef Alaa @Ahmed Khaled Khaled Abdel-sabour Hussien Ahmed @Mohamed Attiya @Israa Abdel Sabour #Graduated_Project #EgSA #NSST #Mars_Exploration #Space_Research #Rover_Prototype #Science_And_Technology #NASA #Space_Mission #Innovation #Soil_analysis #structure_design #Mechanical_Design #Aluminum_casting #Aluminum_Sheets #Linear_Arm #3D_Printed #Mechanical_Analysis #Motion_analysis

A big shoutout to Justin Kruger who became today a #Postdoctoral #Researcher in the #Stanford Space Rendezvous Laboratory (SLAB). His exceptional #PhD #thesis has just been #published and can be downloaded at the link below. Justin did something #monumental for a PhD student by developing new #algorithms for #autonomous #distributed #satellite #swarm #navigation using #visionbased #cameras AND by #successfully #demonstrating them in #orbit on the #NASA #Starling #mission through the Starling Formation-Flying Optical Experiment (#StarFOX). This accomplishment represents the #quintessential #nature of #SLAB. We #conceive, #design, #build, and #fly novel #autonomy stacks for #distributedspacesystems. Kruger, J.; Flight algorithms for autonomous tracking and navigation of distributed space systems using inter-satellite bearing angles; Stanford University, PhD Thesis (2024): https://lnkd.in/dAnJZKAp Table 10.5 from Justin's PhD thesis is emblematic of how we proceed. #Technology #demonstration missions are rigorously defined and accompanied by thresholds and goals on #KeyPerformanceParameters (KPP). Measurement sparsity and on-board software challenges have produced initial difficulties in fulfilling StarFOX objectives. Nevertheless, StarFOX has already demonstrated Capabilities 1 and 2 in flight and has demonstrated Capability 3 using post-processed imagery. Thresholds have also been met for KPPs 1, 2, 4 and 5 in-flight, and for KPP 3 using post-processed imagery. These are the first ever published demonstrations of multi-observer and multi-target angles-only navigation for a satellite swarm in orbit. And this is only the beginning. Way to go Justin!!

🚀 Exciting News! 🛰️ Delighted to announce that our paper titled "Multidisciplinary Design and Optimization of Intelligent Distributed Satellite Systems for Earth Observation" has been accepted in Elsevier IAA Acta Astronautica (IF: 3.5). The article is now In Press, and the Journal Pre-proof is available online. 🌏🛰️ Recent advancements in satellite technology have paved the way for groundbreaking developments in Distributed Satellite Systems (DSS), particularly in Earth Observation (EO) missions. Our research delves deep into optimizing iDSS, focusing on achieving persistent coverage over the vast expanse of the Australian landmass. But designing these intelligent Distributed Satellite Systems (iDSS) is no easy feat. Their complex interactions and unique challenges demand new approaches to Multidisciplinary Design Optimization (MDO). 📌 Key Highlights: 1. Explores the potential of iDSS for LEO satellite constellations. 2. Proposes a Multidisciplinary Design Optimization (MDO) methodology tailored for iDSS. 3. Utilizes tools like OpenMDAO and the Nonlinear Block Gauss-Seidel (NLBGS) iterative solver for optimization. 4. Demonstrates how our optimized iDSS solution promises near real-time persistent coverage over Australia. Thanks to Sir Lawrence Wackett Defence & Aerospace Centre, RMIT University, Khalifa University, University of Luxembourg and SmartSat CRC support in this research endeavor. Ready to dive deeper? Download the paper: https://lnkd.in/dvpPFKDb Roberto Sabatini I Alessandro Gardi I Raja Pandi Perumal I Khaja Faisal #ActaAstronautica #DistributedSatelliteSystems #EarthObservation #MDO #SatelliteTechnology #Innovation #Research #iDSS #SatelliteTechnology #SpaceResearch #Innovation #SmallSats #DistributedSatelliteSystems #MDO #OpenMDAO #Australia #EnvironmentalMonitoring #DisasterResponse #ResourceManagement #SmartSatCRC #AusSpace #SpaceEngineering #SpaceTech #SciTech #FutureOfEO #PersistentCoverage #RealTimeData #GeospatialIntelligence #RemoteSensing #ActaAstronautica #DistributedSatelliteSystems #EarthObservation #MDO #SatelliteTechnology #Innovation #Research #RMITUniversity #KhalifaUniversity #UniversityOfLuxembourg

The Air Force Office of Scientific Research (AFOSR) is proud to announce its support for a groundbreaking project led by Professor Ricardo Sanfelice at UC Santa Cruz. With a $2.5 million grant, this three-year initiative aims to develop advanced digital twin technology and control algorithms for spacecraft capable of cleaning up space debris, repairing, refueling, and decommissioning other satellites. Digital twins are highly detailed computer models designed to mimic the properties of real-world systems, enabling researchers to conduct experiments and analysis in a virtual environment before physical implementation. This project will create digital twins of complex robotic spacecraft, incorporating machine learning for continuous improvement and iteration. A key focus will be on developing next-generation control techniques, such as model predictive control algorithms, to handle extreme scenarios in space. These control systems will enable the robotic spacecraft to perform intricate tasks like grasping and stabilizing tumbling satellites, ensuring safe and efficient operations. By leveraging digital twin technology, the researchers aim to accelerate spacecraft design, reduce costs and risks, and maintain system performance and safety. This research has the potential to revolutionize space operations, paving the way for a more sustainable and secure space environment for future exploration and commercial activities. We are excited to support this innovative project and look forward to the valuable contributions it will make to the aerospace engineering field. Full article here: https://lnkd.in/gUwHC8qm #AerospaceEngineering #DigitalTwins #SpaceDebris #SatelliteOperations #AFOSR #SpaceTechnology #BasicResearch #AFOSRSpaceResearch

🚀 Excited to Share my B.Tech Project on Chandrayaan-3! 🌕 I am a B.Tech student from Dhanekula Institute Of Engineering And Tecgnology, thrilled to present my project inspired by India's Chandrayaan-3 mission. My project, titled "Simulation and Analysis of Lunar Landing for Chandrayaan-3", encompasses several critical aspects of lunar exploration and showcases my dedication to contributing to space science and technology. Project Title:-   Chandrayaan-3 model Project Overview: This project focuses on the simulation and detailed analysis of the Chandrayaan-3 mission's lunar landing phase. Chandrayaan-3 is ISRO's third lunar exploration mission aimed at demonstrating safe and precise landing on the Moon's surface, enhancing our understanding of lunar geology, and paving the way for future lunar missions. Key Objectives: Simulation of Lunar Descent and Landing: Developing a detailed simulation model to replicate the lunar descent and landing of the Chandrayaan-3 lander. Implementing algorithms to simulate various landing scenarios and conditions. Analysis of Landing Dynamics: Studying the dynamics involved in the lunar landing process, including velocity, altitude control, and fuel consumption. Evaluating the impact of lunar surface characteristics on landing safety. Optimization Techniques: Exploring optimization techniques to enhance landing precision and reduce risks. Implementing machine learning models to predict and mitigate potential landing hazards. Technological Innovations: >Autonomous Navigation Algorithms: Developing algorithms for autonomous navigation and hazard detection during the landing phase. >Simulation Tools: Utilizing advanced simulation tools and software (e.g., MATLAB, Simulink) to create realistic lunar landing scenarios. >Data Analysis: Employing data analysis techniques to process simulation data and improve landing strategies. Achievements and Learning Outcomes: Successfully simulated various lunar landing scenarios, demonstrating the critical aspects of the Chandrayaan-3 mission. Gained in-depth knowledge of lunar mission planning, spacecraft dynamics, and autonomous navigation systems. Developed strong teamwork and problem-solving skills, essential for tackling real-world engineering challenges. I am incredibly proud of our work and excited about the future possibilities in space exploration. This project has not only expanded my technical skills but also ignited my passion for contributing to India's space missions. 🔭 Stay tuned for more updates #Chandrayaan3 #SpaceExploration #Dhanekula Institute Of Engineering And Technology #LunarMission #ISRO #BTechProject #SpaceScience #Engineering #Simulation #AutonomousNavigation #FutureEngineers

16U4SBSP mission concept is aimed to demonstrate key technologies for large-scale Space-based Solar Power #SBSP, with a swarm of 16U #CubeSats – in a flight formation approach in comparison with monolithic SBSP concepts. We are proud to have achieved a credible solution which could (1) be applied for in-space demonstration of critical Wireless Power Transfer #WPT technologies in view of future large-scale SBSP systems, (2) provide a pathway for sustainable clean energy supply from space-to-ground in kW-scale SBSP scenarios for emergency needs or commercial use-cases, and (3) be employed in space-to-space WPT use-cases. In a pre-Phase A study funded by the European Space Agency - ESA led by Sirin Orbital Systems AG, together with researchers at Aerospace Centre of Excellence, University of Strathclyde (Massimiliano Vasile, Carmine Clemente, Wail Boumchita, Jinglang Feng) responsible for Mission Analysis and Beamforming and TU Delft | Aerospace Engineering (Angelo Cervone, Stefano Speretta, Mehmet Şevket ULUDAĞ, Caterina Busso) responsible for Spacecraft Architecture, and technical contributions and consultations from Research Institute for Sustainable Humanosphere (RISH) Kyoto University for WPT system, Space Robotics Lab at Universidad de Málaga (Carlos Pérez del Pulgar) for Extensible Hook System Rendesvouz and Docking of a CubeSat Swarm, and 株式会社cosmobloom for Deployable Membrane Antenna system, Rocket Factory Augsburg - RFA for the launch system, and EnduroSat for the full-system integration reviews. The 16U4SBSP study was successfully completed in a workshop held at CDF facilities, ESA/ESTEC on 25/26.04.2024. We sincerely thank CubeSat Systems Unit (TEC-SPC) at the European Space Agency - ESA, for selecting our mission concept within Open Space Innovation Platform (OSIP) campaign 'Innovative Mission Concepts Enabled by Swarms of CubeSats' and guiding us throughout the study: https://lnkd.in/d-4DWDZn #EnergyfromSpace #SOLARIS #SBSP #ESA #Space #CleanEnergy

I will be defending my doctoral thesis next week on Wednesday. If you would be interested in watching, please let me know and I will send you the Zoom link. Title: Low Earth Orbit Spacecraft Slotting: Towards an Implementable Proposal Time: December 6th, 3 pm to 5 pm   Abstract: In recent years, there has been unprecedented growth in the number of proposed Low Earth Orbit (LEO) satellites, driven primarily by large commercial communications constellations. The launch of even half of these satellites would result in an order-of-magnitude increase in active spacecraft traffic, with significant implications for LEO operations. This thesis provides a framework for understanding LEO orbital use in the context of limitations associated with designing orbits for mutual physical compatibility. Intelligently organizing large constellations to efficiently make use of LEO and avoid hazardous conjunctions between on-station satellites offers a way to significantly reduce orbital risk while imposing only minimal burden on satellite operators. This thesis demonstrates technical mechanisms to design efficient mutually-compatible orbits and shells, describes analytical tools to quantify their benefits, explores trade-offs of potential policy implementation pathways, and quantifies reductions to aggregate collision avoidance burden from use of cross-operator compatible orbits. The proposed framework permits quantification of the efficiency of potential orbital shell allocations, the opportunity cost of alternatives, and the amount of remaining uncommitted volume.   Committee: Prof. Richard Linares, Rockwell International Career Development Professor, Associate Professor of Aeronautics and Astronautics, MIT (Chair) Prof. Daniel Hastings, Interim Community & Equity Officer, Interim Vice Provost for Faculty Advancement, and Cecil (1923) and Ida Green Professor in Education of Aeronautics and Astronautics, MIT Dr. Mark Skinner – Senior Project Lead, The Aerospace Corporation Prof. Moriba Jah, MLK Visiting Professor and Associate Professor of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin Mr. Zach Folcik, Technical Staff, MIT Lincoln Laboratory (Reader)  Prof. Kerri Cahoy, Associate Department Head and Professor of Aeronautics and Astronautics, MIT (Reader)

Exploring significant space trends for 2024, including in-orbit manufacturing advancements, new rocket deployments, expanded lunar missions, and the rise of independent space capabilities by nations, offers a glimpse into the future of space exploration. At MAIDANA RESEARCH, our expertise in launching vehicles, engineering design, microgravity research, and digital engineering positions us to contribute meaningfully to these developments. Interested in collaborating? Reach out at [email protected] or visit www.maidana-research.com. #space #spacetechnology #spaceindustry #spaceeconomy #spaceeducation #engineeringsolutions #engineering #physics #rocketscience #rocketry #microgravity #iot #softwaredevelopment #digitalengineering #cad #cae #instrumentation #control #advancedmanufacturing #pocatello #idahofalls #idahostate #idaho #chiangmai #bangkok #thailand #buenosaires #argentina #españa #geneva #switzerland #singapore https://lnkd.in/dWnRV6Yk

Join our Spacecraft systems Course NOW! 🚀 Gain hands-on experience in spacecraft systems: thermal, payload, communication and much more. And enhancing your practical skills essential for real-world engineering projects. 📖 Course Content: 1️⃣ Lecture 1: Spacecraft Fundamentals – Dive into the basics of spacecrafts and their systems. 2️⃣ Lecture 2: Attitude and Orbital Control – This lecture covers the principles and techniques for determining and controlling the orientation and trajectory of spacecraft, including the use of sensors, actuators, and control algorithms. 3️⃣ Lecture 3: Payload Systems – This lecture explores the different types of spacecraft payloads, such as scientific instruments, remote sensing devices, communication systems, and navigation equipment, along with their design, integration, and data management. 4️⃣ Lecture 4: Communication, Power & Thermal Systems – This lecture discusses the critical systems required for spacecraft operations, including communication links, power generation and storage, and thermal control to ensure the spacecraft’s functionality and longevity in space. 5️⃣ Lecture 5: Q/A Lecture – To answer any questions you may have and assist you with any inquiries regarding the course topic. ℹ More Info: • course schedule: 22nd of July to 20th of August • recourses: A course handbook containing all the taught topics and resources will be provided. 🛒 Book your seat now: https://lnkd.in/dxWAxfF3 📧 Email us for any inquiries: [email protected] #art #space #rockets #satellite #ksa #uae #moon #education #news #partnership #deal #space_for_all #fadaa_program #students #university #ground_station #engineering #sponsorship #horus4 #course #oman #muscat #business #summit #conference #education #spacex #elonmusk #nasa #technology