Recent content by GNCstudent

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    Graduate From RTN reference frame to ECI and orbital elements

    - Also the chaser has no initial velocity (it's zero)
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    Graduate From RTN reference frame to ECI and orbital elements

    Some data and simplifications, that can be used here : - the target's orbit is circular - the RTN position of the chaser is (30;10;10) m - the mass of the chaser is 1000kg and the mass of the target is 8000kg - the target has an altitude of 800e3 m
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    Graduate From RTN reference frame to ECI and orbital elements

    Hi all, I'm curently meeting the following problem and can't figure it out by myself. Assume we have to vehicles in space, a target and a chaser spacecraft . The target spacecraft defines the RTN frame of reference. Given the position and velocity of the chaser in RTN-coordinates, how can I...