
Mechanical disturbances from spacecraft equipment, such as reaction wheels, can couple into the satellite structure and affect sensitive payloads. Previous work at OHB has investigated methods for estimating reaction-wheel parameters from measured waterfall plots.
The purpose of this thesis is to develop a simple and cost-effective experimental setup for characterizing relevant dynamic parameters and evaluating structural or damping improvements.
The proposed concept is a flexible plate or table supported by springs and instrumented with accelerometers and/or force sensors. The work will combine analytical modelling, finite element analysis, and measurement data to identify parameters such as stiffness, damping, and modal properties.
The long-term objective is to establish a fast in-house method for comparing structural and damping concepts before formal qualification testing.
Possible future applications include evaluating bracket designs, elastomeric damping concepts, and other structural interfaces.
The thesis will focus on developing and validating a method for identifying mechanical parameters from vibration measurements.
The student will design and model a simplified test setup, define suitable measurement methods and investigate how sensor data can be translated into physical parameters of the test object. The method will first be verified using simulated data with known parameters.
The core scope includes modelling, parameter identification, test-jig design and uncertainty assessment. Depending on progress, available hardware and budget, the thesis may also include manufacturing and experimental testing of the setup.
The thesis will follow a top-down approach, starting with a deliberately simple and well-understood mechanical system. Once the modelling and parameter-identification method has been validated, individual design changes can be introduced and their effect quantified relative to a baseline.
If time and resources allow, the work may also include manufacturing of the test jig and validating the method experimentally using a motor, engineering model or available reaction wheel.
A secondary application may be investigated using impact-hammer excitation to measure transfer functions through brackets or structural interfaces.
Preferred:
Successful thesis work may also open a path towards future employment within the Mechanical & Thermal team at OHB Sweden.

OHB Sweden is a Swedish provider of space systems and develops, builds, tests and operates satellites for different kinds of space missions within communications, earth observation, space research and exploration. From low-orbiting satellites via geostationary ones and all the way up to interplanetary missions.
OHB Sweden is a member of the OHB AG Group (ISIN: DE0005936124, Prime Standard) which currently employs over 2.200 people in its “Space Systems” and “Aerospace + Industrial Products” business units. Within this array, OHB Sweden AB belongs in Space Systems.
Spacecraft heritage includes satellites such as Freja, Astrid 1, Astrid 2, Odin, SMART-1 and the PRISMA system with its two satellites Mango and Tango. All current smallsats are based on the InnoSat microsatellite platform like: GMS-T, MATS, AWS, EIS, GARAI