Essays about: "låg omloppsbana"
Showing result 1 - 5 of 11 essays containing the words låg omloppsbana.
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1. Space Rider System: GNC and System Model Improvements
University essay from KTH/RymdteknikAbstract : As part of a continuous trend of the space sector for obtaining higher performance space science and Earth observations, there is an increasing demand for higher requirements in pointing accuracy and disturbance prediction. The Space Rider System (SRS) is a Low Earth Orbit (LEO) reusable vehicle that aims at answering to that demand. READ MORE
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2. Error Injection Study for a SpaceFibre In-Orbit Demonstrator
University essay from KTH/Skolan för elektroteknik och datavetenskap (EECS)Abstract : The space electronics sector is shifting towards the New-Space paradigm, in which traditional space-quali_ed and expensive components and payloads are replaced by commercial o_-the-shelf (COTS) alternatives. This change in mentality is accompanied by the development of inexpensive cubesats, lowering the entry barrie in terms of cost, enabling an increase in scienti_c research in space. READ MORE
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3. Comparison of Control Approaches for Formation Flying of Two Identical Satellites in Low Earth Orbit
University essay from KTH/RymdteknikAbstract : Formation flying of satellites describes a mission in which a set of satellites arrange their position with respect to one another. In this paper, satellite formation flying guidance and control algorithms are investigated in terms of required velocity increment Delta-v, and tracking error for a Chief/Deputy satellite system. READ MORE
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4. Conceptual Design of an Air- launched Multi-stage Launch Vehicle
University essay from KTH/FysikAbstract : In the present thesis, the objective was to find the maximum amount of payload mass that can be put into a 500 km polar orbit by a 1400 kg air-launched multi-stage rocket launched from a fighter jet platform. To fulfill the objective an algorithm incorporating several modules was developed. READ MORE
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5. Conceptual Design of an Air- launched Multi-stage Launch Vehicle
University essay from KTH/FysikAbstract : In the present thesis, the objective was to find the maximum amount of payload mass that can be put into a 500 km polar orbit by a 1400 kg air-launched multi-stage rocket launched from a fighter jet platform. To fulfill the objective an algorithm incorporating several modules was developed. READ MORE