RS-39 daily summary

Summary of the satellite “Chibis-M” on the first turn, presented by the ground control Kaluga

MC Branch, “Chibis-M” of THC occurred on schedule at 23:18:30 UTC (Jan 24). Immediately after turning on the presence of a signal was received at the remote reception center in Krasnoyarsk, where he was seconded to the representative NILAKT. The signal was heard with a good volume. On the first circuit within sight of the ground control Kaluga was installed two-way radio and radio were tested both. Commands were issued, which allowed to assess the state of power supply systems, state radio systems and other onboard systems. According to our data radio system and power system are functioning normally. Was checked battery voltage, current consumption equipment, modes of operation of the devices, solar panels work. Scan results are normal.

The next stage of the study was conducted orientation and stabilization systems. On the first turn produced:

– Reading of orientation sensors: magnetometers, sun sensors, the angular velocity in order to verify their efficiency, as well as estimates of the initial angular velocities of the satellite after its separation from THC;
– Control settings and the calibration parameters of orientation and stabilization by comparing them with pre-values ​​in the world;
– To set and monitor performance of the algorithm of satellite stabilization – damping of the angular velocity of rotation with a rotation of the solar panels at the sun. To implement these checks had been formulated a sequence diagram issuing commands, which was implemented in the first communications. The result is the following:
– On the first turn of the telemetry revealed that the initial angular velocity according to the testimony of CRS (angular velocity sensor) after the removal of THC was, in absolute value, of about 4 deg / sec
– Turns on all clear that the magnetometer readings, according to the telemetry data, change adequately,
– On the first, second and third turns according to the testimony of two-level satellite has a constant in magnitude and direction of the angular velocity, which suggests that the algorithm is the damping of angular velocity is not operated;
– The control system configuration orientation held on the third circuit showed that the wrong set of satellite stabilization mode, which is the reason for the lack of damping of angular velocity in the first stage, to address the issue on board were transferred to the appropriate commands to enable the desired mode of stabilization;
– Further control on the fourth circuit, showed that the damping is implemented, the angular velocity is reduced by an order. It shows performance of the algorithm pre-sedation
– The first circuit has the problem with the solar sensor 209, as expressed in the fact that the testimony with him, “zaliplo” and did not change regardless of whether the sun comes into its field of view or not. Problem solved removing the power supply and all sensors in conjunction with solar restart the procedure for their interview;
– On the fourth circuit board laid on the actual orbital elements, verified that they are received and properly used for the prediction of the orbit on board the satellite.
– In front of the domain of “Deaf” is de-energized coils BUSOS to conserve power until the next nearest session.

Plans for the next sessions for orientation and stabilization system:

– Calibration of the magnetometer;
– Calibration of solar sensors;
– Inclusion of a three-axis attitude determination algorithm using a magnetometer and sun sensor local algorithm;

At the turn of a signal has been switched off 10:30:23 presence in order to save battery power.

Management activities are conducted on the satellite ground complex NILAKT DOSAAF in the city of Kaluga, and a remote ground complex NILAKT located in Krasnoyarsk.

Starting from the time of separation and to present the signals MC “Chibis-M” watching amateurs around the world. At the first turn of reports of reception of a signal at the frequency of the presence of 435,315 MHz have been obtained from hams, Ust-Kut and Yakutsk, Khabarovsk and Kamchatka on radio. After this, began to receive information about the reception of signals from Japan, Australia, New Zealand, Argentina, India, the USA and Western Europe.

http://chibis.cosmos.ru/

RS-39

00:59 UTC   435.315 MHz

RS-39/MP3:rs39-0125-UTC0059-1

US    135     IBS   117     USUN  24      ISUN  5    ITXA  0       ITXB  0       TTXA  132     TTXB  131
TNAP  128     TAB   133     MSEP  0       MCON  5    SMA   150     SMB   166     MRXA  2       MRXB  2  

OnBoard Voltage:                     13.5 V
OnBoard Current:                     1.17 mA
Charge Voltage from Solar battery:   2.4 V
Charge current from solar battery    0.05 mA
D.C. current of the 435 MHz TX A:    0 mA
D.C. current of the 145 MHz TX B:    0 mA
Temperature of the 435 MHz TX A:     4 °C
Temperature of the 145 MHz TX B:     3 °C

Temperature of the Navigation Unit:  0 °C
Temperature of onboard battery:      5 °C
operational Mode of power supply:    0
operational mode of controller:      5
operational mode of channel A:       150
operational mode of channel B:       166
operational mode of RX A:            2
operational mode of RX B:            2
PROGRESS-M 13M
1 37857U 11062A   12024.77684352  .00056776  00000-0  24725-2 0   883
2 37857 051.6454 126.6672 0010468 237.3762 226.7793 15.21618116 13479

Heard the RS-39 CW telemetry during the 4:14 UTC pass over India. Recording can be found at http://www.vu3tyg.addr.com/RS-39/ . The signals were strong and I was following the keps of the Progress M13 M cargo ship. The RS -39 CW signals were heard 2 minutes after Progress M13 in range.

73 Nitin [VU3TYG]

CHIBIS – RS-39 ready to go

On November 2, 2011 cargo ship “Progress M-13M”, which also delivered microsatellite “Chibis-M”, was docked with ISS. The main purpose of “Chibis-M” is the study of physical processes in the vicinity of the lightning, during which the Terrestrial Gamma Ray Flashes (TGFs) are generated. TGFs are likely produced by beams of very energetic electrons, which are accelerated in the intense electric fields generated by large thunderstorm systems.

The deployment of “Chibis-M” in a circular orbit of 500 km will take place during the final phase of “Progress M-13M” operation. According to the plan of the Russian Space Control Centre, undocking of “Progress M-13M” will occur at January 23, 22:10 UTC and after two corrections it will be positioned at 500 km orbit. At January 24, 23:19 UTC “Chibis-M” will separate. Beside scientific data “Chibis-M” will transmit service telemetry (the housekeeping parameters) in the beacon format on 435.315 or 435.215 MHz CW and has the designation of RS-39. The format of data is typical for RS satellites.

The telemetry of RS-39 can be easily received directly by schools and colleges for educational outreach purposes. This telemetry will give details of the spacecraft’s health – battery voltages and temperatures of critical units. In combination with orbital data such information will be useful as the curriculum for student lessons. The main site for CHIBIS managed by Space Research Institute of RAS is here http://chibis.cosmos.ru. The mail address for connection with radio amateurs around the world will be opened very soon on site mentioned above.

The team of RS-39 will very much appreciate any reception reports of “Chibis-M” voice. Special attention is requested for the first orbits as these are outside of control stations for “Chibis-M”. Each report will be confirmed by special QSL card. They issued the special e-mail address for the CHIBIS-M project to collect all messages from amateurs:

amateur-rs39@chibis.cosmos.ru

Hope to hear new RS-39 very soon!
73! RW3DZ, UA3XBU