- Article
Estimating the Inertia Tensor Components of an Asymmetrical Spacecraft When Removing It from the Operational Orbit at the End of Its Active Life
- A. V. Sedelnikov,
- D. I. Orlov,
- M. E. Bratkova and
- E. S. Khnyryova
The paper presents a method for estimating the inertia tensor components of a spacecraft that has expired its active life using measurement data of the Earth’s magnetic field induction vector components. The implementation of this estimation me...