Symmetrized approach to presentation the inertia tensor for composed asymmetric vehicles of aerospace engineering

The new approach to the algorithm of inertia tensor components transformation procedure is proposed. This inertia tensor describes the state of combined asymmetric space vehicles and orbital inhabited stations while spatial turn and coordinate system transfer. Discussed approach is based on the application of matrices which are isomorphic to the quaternions. This approach advantage is a possibility to obtain algorithms suitable for realization on PC with simultaneous control of calculation results using invariant relationships.