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interactions. Orbit dynamics evolve over a longer timescale compared to the rapid dynamics of attitude and GNC systems. Simulating these subsystems together requires sophisticated numerical methods to maintain
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-order differentials. Differentiable wind models for accurate re-entry simulations. High-order State Transition Tensors usages and efficient computation. Manoeuvre detection and estimation of non
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, structural, dynamics, etc.) facilitating a fast, rigorous and robust requirements verification process within the MBSE collaborative environment. Your areas of research will be chosen both based on your own
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