Essays about: "Orbit Determination"
Showing result 1 - 5 of 29 essays containing the words Orbit Determination.
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1. Conjugate Heat Transfer Analysis of HPGP Thruster
University essay from Luleå tekniska universitet/RymdteknikAbstract : This master's thesis was conducted in collaboration with ECAPS, where a conjugate heat transfer analysis on their High Performance Green Propulsion (HPGP) 22N thruster was done. ECAPS is a Swedish propulsion company specializing in green propulsion. They develop thrusters for spacecraft orbit and attitude control, utilizing the propellant LMP-103S. READ MORE
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2. Real-Time Navigation for Swarms of Synthetic Aperture Radar (SAR) Satellites
University essay from Luleå tekniska universitet/RymdteknikAbstract : The pursuit of precision and flexibility in satellite missions has led to an increased number of formation flying missions being developed. These systems consist of multiple satellites flying at close distances (from a few kilometres to a few meters) to achieve common objectives. READ MORE
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3. Initial Orbit Determination of Resident Space Objects From A Passive Optical Imaging System: : Application to Space Situational Awareness
University essay from Luleå tekniska universitet/RymdteknikAbstract : The probability of satellite collisions and disintegrations cluttering the near-Earth orbital environmentis ever-growing. This is especially true for the congested Low Earth Orbit (LEO) regime; once a critical density of objects is reached, a collisional cascading is projected to generate runaway growth of theorbital population. READ MORE
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4. Testing for verification and validation of an onboard orbit determination system exploiting GNSS : A nanosatellite application for HERMES-SP
University essay from KTH/Skolan för elektroteknik och datavetenskap (EECS)Abstract : When developing products for space, including nanosatellites, the verification and validation process is a mandatory part of any project conducted within the European space industry. Within such a process, testing is a method for verification and validation. READ MORE
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5. Hardware-In-the-Loop Simulation of MIST Attitude Determination and Control System
University essay from KTH/Skolan för elektroteknik och datavetenskap (EECS)Abstract : The MIST(MIniature Student saTellite) project is a 3U CubeSat developed by student teams at KTH Royal Institute of Technology in Stockholm. One of the fundamental systems of the satellite is the Attitude Determination and Control System (ADCS), re sponsible for estimating and correcting the satellite’s orientation using magnetic fields and sun sensors. READ MORE