CUTE-I Telemetry
Analysis |
2005/07/12 Updated |
Analyzed results of CUTE-I telemetry are reported here. |
![]() ![]() ![]() ![]() |
# Motion Right After Separation -> 2003/08/08 Completed |
At 300 seconds after the separation, three monopole antennas of CUTE-I were successfully deployed. The following graphs show angular velocity at near the deployment time. Precise antenna deployment time is 303s. The angular velocity starts to change at 303s. The antennas are coiled around b2-axis(in CUTE_Frame) of CUTE-I, so the antennas deployment influences the rotation around b2-axis. The following graph certainly indicates the effect of antenna deployment.![]() Definition of CUTE-I's Coordinates ![]() Angular velocity at near 300sec after separation from gyro sensor ![]() Euler parameter at near 300sec after separation |
# Long Term Temperature Change -> Now on mission |
2003.7-2003.8![]() Temperature history(2003.7.1-2003.8.31) |
2003.7-2004.5![]() Temperature history(2003.7-2004.5) |
2004.5-2004.7 ![]() Temperature histroy(2003.7-2004.7) |
2003.7-2005.7 (05/07/12 updated)![]() Temperature history(2003.7-2005.7) |
# Demonstration of communication protocol-> Now on mission |
![]() |
# Temperature Fluctuation along Orbit-> Completed |
![]() Definition of wall’s number ![]() Temperature Fluctuation in Orbit (Aug 20) |
# Sun Sensor Test-> Completed |
|
# Motor Test-> Completed |
|
# Check of Onboard Memory(SRAM) -> Completed |
under construction |