Definition of Dynamic Characteristics of ISS (Tenzor (Tensor)) - 01.09.14
Science Objectives for Everyone Information Pending
Science Results for Everyone Information Pending
Sponsoring Space Agency
Russian Federal Space Agency (Roscosmos)
ISS Expedition Duration:
November 2000 - October 2004
Previous ISS Missions
Development test of the techniques defining and updating ISS dynamic characteristics required for improvement of attitude determination accuracy, prediction of the onboard systems functionality and qualitative performance and analysis of science experiments.
Angular rate vector gyrometer, Fixed star meter to measure angular rates and station location.
Reception of integrated information from the ISS guidance navigation and control system (GNC) sensors and TV cameras of spacecraft maneuvering near the ISS (Shuttle, Soyuz, Progress) to determine dynamic characteristics of the ISS (ratios of moments of inertia, aerodynamic characteristics, center of gravity of the ISS, etc.). Updating of mathematical models of the ISS onboard systems used for flight control.
- Coordinating Scientific and Technical Council of the Russian Space Agency [Russian]
- Energia - Science Research on the ISS Russian Segment