Paper Category: Simulation, Modeling
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Broadband vibration isolation in a deployable telescopic baffle exploiting post-buckling thrust tube dynamics
Stray light suppression is a primary consideration for high-performance optical instruments, yet the necessary baffle dimensions often conflict with launch volume restrictions. Existing solutions necessitate a trade-off: motorised telescopic mechanisms provide structural rigidity but incur significant mass, complexity and cost penalties. Flexible deployable shrouds, whilst volumetrically efficient, lack the deterministic geometry required for high-precision optical…
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A Coupled Analytical-Simulation Approach to Redundant Small Spacecraft AOCS
Missions including close-proximity operations and docking (CPOD) as well as in-orbit servicing are redefining the capabilities of small spacecraft. As a result, attitude and orbit control systems (AOCS) requirements have evolved to include not only attitude maintenance, but also 6-DoF translation and rotation. Cold-gas thruster arrays are key to these capabilities, but optimising their design…
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Design and Analysis of a Composite Satellite Bus for VLEO Applications
The increasing interest in Very Low Earth Orbit (VLEO) missions has highlighted the need for lightweight satellite structures capable of withstanding demanding launch and operational environments. The main objective of this research focused on the development and structural validation, by finite element method (FEM) analysis, of a composite dominated microsatellite bus architecture suitable for VLEO…
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AI-Based Navigation for Lunar Satellites in VLLO
This paper presents the design and preliminary validation of the Lunar Intelligent Navigation via Neural Architecture (LINNA) payload, a technology demonstration integrated into the SelenITA mission—Brazil’s first lunar CubeSat. The experiment is motivated by the future needs for autonomous state estimation in the Very Low Lunar Orbit (VLLO) regime, where Mascon-induced gravitational anomalies challenge traditional…
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A Modular Open-Source ADCS Framework for Small Satellite Development and Testing
Advanced attitude determination and control (ADCS) techniques are often difficult for small satellite teams to adopt due to tightly coupled implementations and the need to rapidly evaluate alternative architectures. Evaluating prospective ADCS options may require significant modification of existing code for specific actuator combinations, sensor hardware, orbits, mission goals, and control laws. Existing options are…
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Design, prototyping and mechanical testing of a trifilar deployable helix antenna for CubeSat applications
Deployable helical antennas are often used in space in the VHF and UHF transmission bands because they provide high gain, large bandwidth, and high directivity with circular polarization while maintaining relatively low fabrication complexity. Usually, these deployable antennas are composed of a main foldable, non-conducting isolated structure which acts as the helicoid support for the…
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CubeSat ISR Constellation Mission Tailoring
This paper presents a modelling framework for Intelligence, Surveillance & Reconnaissance (ISR) CubeSat constellation combining optical payload and Software Defined Radio (SDR). The concept satellite is 8-16U depending on the payload resolution and presence of warm-gas propulsion allowing for orbital changes and station keeping extending the operational time. Deployed in 500-km Sun-Synchronous Orbit (SSO), the…
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Space weather forecasting using SARIMA
Solar fluxes and geomagnetic activity influence the temperature of the air, and consequently the density. These phenomena are hard to predict because of their highly nonlinear and stochastic nature. However, they have significant effects on LEO space missions and orbital decay time estimations, since air drag is one of the major perturbations in this region.…