|
USED SCIENCE HARDWARE:
- Sensors of the guidance navigation and control
system (GNCS) measuring angular velocities of the
station;
- Attitude sensors measuring the station attitude;
- Sensors measuring kinetic moment of the gyrodynes
- Sensors measuring rotation angles of the gyrodyne
frames
- Magnetometers measuring the magnetic field value
- Russian
and foreign accelerometers.
|
|
PURPOSE:
Consolidated study of the ISS dynamic characteristics;
parameters defining a space position of scientific
devices and attitude sensors with respect to the
station hull deformation; parameters of magnetic
and microgravity disturbances on board the station.
OBJECTIVE:
Specify dynamic parameters of the station, position
of sensitive axes of the attitude sensors and devices,
microgravity and magnetic disturbances.
EXPECTED RESULTS:
Acquisition of initial data required for development
of mathematical models of magnetic disturbances and
micro g-loads, database on hardware effect on levels
of magnetic disturbances, as well as dynamic operations
effect on a level of micro g-loads. These models
and databases are needed to plan scientific experiments
on the ISS RS and account for station partners’ requirements.
EXPERIMENT RESULTS:
Telemetry measurement information from the flight
sensors and scientific devices received from the
station.
|
