Available Master's Thesis in Space Systems and Sensor Technologies

• J
  • jotne_5: AI-Driven On-Board Edge Processing for Real-Time mm-Sized Space Debris Detection
  • jotne_4: LLM-Assisted Automated Flight Operations Procedure Generation and Validation for CENSSAT-1
  • jotne_3: Physics-Based Machine Learning Framework for Solar Array and Payload Sensor Degradation Modeling and Life Expectancy Prediction
  • jotne_2: LLM-Based Satellite Health Management and Event Analysis
  • Jotne_1: Dynamic Payload Operation Scheduling & Power Prediction Framework for CENSSAT-1

• G
  • GRNS_4: SiPM Characterisation
  • GRNS_3: SiPM readout electronics
  • GRNS-Spin-off: moisture monitor
  • GRNS_1: Data processing pipeline for Lunar ISRU instrument (GRiNS)
  • GRNS_2: Field test of GRNS instrument, aiming to the Moon

• R
  • RP_1: Rocket launch exhaust plumes

• M
  • MA_1: Martian aurora variability

• C
  • Component-Testing_3: TID testing of Si photomultipliers
  • Component-Testing_1: DD/TNID test of Silicon Diodes
  • CENSSAT-1_Rad_1: Calibration and Characterisation of the ASTRA-LEO Detector
  • CENSSAT-1_Rad_3: Modelling and Simulation of ASTRA-LEO Detector Performance
  • CENSSAT-1_Rad_2: Operations Planning and Science Readiness for ASTRA-LEO
  • CENSSAT-1_SYS_2: Satellite operation concept
  • CENSSAT-1_SYS_3: Systems Engineering, Visualisation
  • CENSSAT-1_SYS_4: SatNOGs ground station
  • Component-Testing_2: Space Components Radiation Testing (TID or SEE)

• F
  • FFI_1: Design of Spacecraft Attitude Guidance and Control System for Imaging while Tracking Accessible Curves on a Surface
  • FFI_2: Space Robotics for In-Orbit Manipulation of Target Spacecraft
  • FFI_3: Using Norsat-4 to study the Influence of observing conditions on the detectability of ships
  • FFI_4: Satellite concepts using available radio signals for detection of ships and/or spacecraft

• S
  • SpaceSys_1: In-orbit servicing for sustainable space operation
  • SpaceSys_2: Space Debris Mitigation