Method for determining the state variables of a moving rigid body in space
OwnerRoland Strietzel, Karl-Hermann Kolkinventors
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OwnerRoland Strietzel, Karl-Hermann Kolkinventors
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A method for determining the state variables of a moving rigid body in space, in particular for determining the position and attitude of a spacecraft during an approach and docking maneuver. The task of finding a new possibility for determining the state variables of a moving rigid body, which delivers a simplification and ensures a higher level of reliability in calculating the state variables is accomplished according to the invention in the case of a method for determining the state variables of a moving rigid body by determining the state variables of the moving body with the aid of a state observer, in which case measured data of scannings of a plurality of retroreflectors in space are processed by an internal memory model to produce the desired output signal of the state variables of the moving body, starting from set initial values and known system parameters implemented in operators, a current state vector of the moving body being calculated as an estimate, and being adapted to the actual attitude characteristic and movement characteristic of the body with each measuring cycle by a correction, such that after a specific number of measuring and calculating cycles the estimated values track the actual movement data of the body in space and are used as state variables of the body.
A method for determining the state variables of a moving rigid body, such as relative position and attitude as well as translational and rotational speeds, in particular for a movement of approach to another body employing measured data provided by an active sensor, the measured data being derived from at least three rectroreflectors whose configuration on the other body is known and is assigned in a defined fashion to a body-specific coordinate system of the other body, comprising the steps of:
Dependencies are inferred from the claim text.