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- W2756867319 abstract "Australian researchers and Heliaq Advanced Engineering are developing reusable small satellite launch systems. These systems include rocket boosters which change configuration during flight to return to their launch position. Simulating these multivehicle systems presents a number of unique challenges. System models must consider atmospheric and orbital simulations for the payload and return-to-home components. Simulations must handle rocket-based vehicles as well as fixed wing aircraft. A pseudo-five-degrees-of-freedom system model has been developed using OpenModelica. The model simulates the launch vehicle from launch to orbit in a single simulation with parameters that can be tracked across all stages of the flight. The system includes generic models for vehicles that can be implemented as launch vehicles, free falling objects, or as fixed wing aircraft. Future work will expand the model to full six-degrees-of-freedom, the mechanical interactions between vehicles, and internal effects such as structural loads and fluid flow effects." @default.
- W2756867319 created "2017-10-06" @default.
- W2756867319 creator A5019906613 @default.
- W2756867319 date "2017-01-01" @default.
- W2756867319 modified "2023-09-26" @default.
- W2756867319 title "Simulation of a small satellite launch system with fly-home components" @default.
- W2756867319 hasPublicationYear "2017" @default.
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