JAQAR Astrodynamics Package - ESA
JAQAR Astrodynamics Package - ESA
JAQAR Astrodynamics Package - ESA
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R # x $ y02 2DATO Test Cases• Two optimisation of trajectory (ascent and descent testcases) are presented.• Examples are given for a lift launch vehicle and Lunardescent vehicles.• The obtained results are compared to referenced data.
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