Sökning: "Attitude controller"
Visar resultat 21 - 25 av 35 uppsatser innehållade orden Attitude controller.
21. Black-Box Modeling and Attitude Control of a Quadcopter
Master-uppsats, Linköpings universitet/ReglerteknikSammanfattning : In this thesis, black-box models describing the quadcopter system dynamics for attitude control have been estimated using closed-loop data. A quadcopter is a naturally unstable multiple input multiple output (MIMO) system and is therefore an interesting platform to test and evaluate ideas in system identification and control theory on. LÄS MER
22. Attitude Determination and Control of the CubeSat MIST
Master-uppsats, KTH/Farkost och flygSammanfattning : The ADCS concept in MIST reects the limitations of the CubeSat in terms of space, power and onboard computer computational capability. The control is constrained to the use of only magnetic torquers and the determination to magnetometers and Sun sensors in spite of the the under-actuation and underdetermination during eclipses. LÄS MER
23. Model-Based Design, Development and Control of an Underwater Vehicle
Master-uppsats, Linköpings universitet/ReglerteknikSammanfattning : With the rising popularity of ROVs and other UV solutions, more robust and high performance controllers have become a necessity. A model of the ROV or UV can be a valuable tool during control synthesis. The main objective of this thesis was to use a model in design and development of controllers for an ROV. LÄS MER
24. Development of Star Tracker Attitude and Position Determination System for Spacecraft Maneuvering and Docking Facility
Master-uppsats, Luleå tekniska universitet/RymdteknikSammanfattning : Attitude and position determination systems in satellites are absolutely necessary to keep the desired trajectory. A very accurate, reliable and most used sensor for attitude determination is the star tracker, which orient itself in space by observing and comparing star constellations with known star patterns. LÄS MER
25. Attitude and Orbit Control During Deorbit of Tethered Space Debris
Master-uppsats, KTH/Farkost och flygSammanfattning : Due to the unsustainable space debris environment in Low Earth Orbit, debris objects must be removed to ensure future safe satellite operations. One proposed concept for deorbiting larger space debris objects, such as decommissioned satellites or spent upper rocket stages, is to use a chaser spacecraft connected to the debris object by an elastic tether, but the required technology is immature and there is a lack of flight experience. LÄS MER