Cubesat Full
Cubesat Full
Cubesat Full
Asem ELARABI , Akram ELKASEH , Abdurrahim ABUGHUFA ), Said BEN RABHA , Ahmed TURKMAN , Mahdi
ALAYEB
)
The Libyan Center for Remote Sensing and Space Science, Tripoli, Libya.
asemelarabi@gmail.com
Desertification is one of the main problems threatening the Libyan agriculture. The major environmental hazard in
this area is sand encroachment from the south direction towards the north directions. Deforestation is another
important threat of agriculture in Libya, especially in the recent years, with no lawful authority to control the chaotic
deforestation process, huge areas of forests are threatened to become unorganized farms, houses and buildings. By
building our own Cube-Sat , its images could be used to observe and monitor deforestation, desertification, and to
control the uncontrolled increasing violation of green lands and illegal buildings.
In our mission, we are planning to develop and fabricate a cube-sat –initially called “LCRSat-I” – to monitor the
agricultural cover of Libyan lands. The satellite mission aimed at monitoring and assessing of desertification in
southern Libyan land, deforestation in the north, and random build houses and buildings. In addition, it will be used
to investigating the potential use of remote sensing and GIS in assessing and monitoring sand encroachment and
vegetation degradation as desertification indicators in the semi-arid environment. These valuable data will help the
government to initiate platform data bases which can be used in the development of Libya infrastructure.
Fig. . Landsat images of Tripoli: top image at 1989 and bottom image
at 2003.
If we compare what is inside the two images, we will see a
clear deforestation due to the unjust use of private land and
cutting down trees in many regions. Randomly built houses
were fabricated after green-lands and forest were destroyed by
human being.
Fig. . Landsat images of south east Tripoli: top image at 1989 and
bottom image at 2003. . LCRsat-I Satellite Subsystems Overview
In Libya, desertification and deforestation are main According to the specification, a standard Cubesat satellite
environmental hazards that facing the government. As most of is 10 cm cube weighing at most kilogram. Currently, up to
the land is covered with big SAHARA, both factors can affect three such cubes may be combined and thus creating a single
the agriculture sector immediately. satellite of dimensions 10cm × 10cm × 30cm with mass of 3
There are natural and human factors that play a major role in kg.
the raise of desertification and deforestation in the Libya, LCRsat-I will be within the standard specification and the
configurations of ground segment, space segment and . . Attitude Determination and Control System
launching methods that would be most cost-effective will be The ADCS system is the most crucial system in the sense
identified. that any spacecraft or instrument has to be oriented towards a
specific target and toward the ground station while keeping
. Ground Station and Antenna the orbit parameters in certain limits. This can be achieved
A basic ground station consists of hardware and software to using sensors for acquiring spacecraft attitude and position as
transmit and receive data reliably. The ground station includes well as orientation and after performing on board calculation
transmit and receive antennas, a computer programmed with or receiving commands from the ground the spacecraft makes
orbital-prediction software compatible with the hardware, and use of actuators to achieve the desired trajectories.
transceiver to transmit and receive data. The most common sensors used in ADCS are: the sun sensor,
With the radio band determined to be in the amateur band, the Earth sensor, star track, magneto-meters, gyroscopes, and
ground station antennas will be chosen to be a GPS.
commercial-of-the-shelf rotator VHF and UHF antennas with Attitude control can be performed passively using magnets
high gain. and gravity gradient, or actively performed by a control
mechanism such as gas thrusters, three-axis magnetic torque
. . Power Supply Subsystem coils, or by momentum /reaction/inertial wheels.
The main functions for the power system are provision, To date Commercial Cubesat ADCS modules are available
storage, distribution and control of power to other satellite from the market including sensors, actuators and processors,
subsystems such as RF communication, Attitude Determine such modules as the ones from ClydeSpace company will be
and Control system (ADCS), image processing, deployable used in LCRsat-I Cubesat.
mechanism actuation. Power budget must ensure that the
payload and all Cubesat subsystems have the power they need . . Optical Payload
during the lifetime of the satellite. The satellite power systems To fulfill the photography mission of LCRsat-I, a small
include electrical power system, battery assemblies, and commercial camera is used. Optical payload consists of
deployable solar cells. commercially available high resolution single lens reflex
The Electrical Power System (EPS) is responsible for gathering camera lens, processor and memory. For typical satellite
power from solar panels, storing into batteries and distributing orbiting at around 700 km altitude, the expected equivalent
it for whole system. LCRsat-I will be orbiting in Low Earth area in a 3 mega pixel image is a 50 × 70 km. The expected
orbit (500km – 700km) in such a way that it will be in eclipse pixel resolution is tens of meters for a camera consists of a
during about 30% of the orbital period. Part of the captured 2048× 1536 matrix of pixels, enabling the identification of
solar energy must be kept in a battery in order to return it to the geographical features and even a large construction at the
subsystems during the eclipse. EPS has to control, distribute ground.
and regulate power for subsystems and to balance power
requirements and generation during eclipse and sun phase.
There will be five sides covered with solar cells, two solar cells
per side of the satellite that are connected serial and different
sides are connected parallel to each other. Two Lithium ion
rechargeable batteries connected in series will be used as a
second source of power.
. . Communication
The primary goal of the communication subsystem is to
provide a link to relay data findings and send commands to
and from the Cubesat. Analog digital data collected by the
sensors and payload must be relayed to the ground station via
the telemetry system.
Command and uplink portion is another aspect of the
communication subsystem. All incoming signals from the
ground will be received by the antenna, encoded, and Fig. 1. Commercial camera on board for Cubesat .
processed, errant signals will be discarded.
A transceiver is a single board housing both a transmitter and Similar high resolution satellite camera with interface board
receiver circuit. The transceiver converts data from the on works at visible light spectrum and accessible high accuracy
board computer (OBC) into a form that can be sent to ground will be used to image the extent of sand encroachment and the
stations via a carrier signal. The most common Transceivers vegetation deterioration during satellite life time.
for CubeSats operate in both the UHF and VHF bands. This
allows the use of the VHF band for downlink and UHF band LCRsat-I will use a modified commercial of the shelf structure
for uplink or vice-versa. consists of a 1U skeletonized aluminum cage. Thermal
A commercially available high speed data rate ISIS UHF / subsystem maintains the satellite temperature within
VHF transceiver will be used in our satellite. acceptable limits.
Thermal control subsystems can be used actively and Osaraetin, I., Retherford, L., Scarito, M., Nanosatellite for earth
passively, active systems such as heat pumps, electric heaters environmental monitoring: The MicroMAS project. Microwave
Radiometry and Remote Sensing of the Environment, IEEE. 2012,
or coolers, have the capacity to turn on and off to adjust the ISBN: 978- - -
temperature of the satellite subsystems, whereas passive . “Student satellite to be launched” BBC news:
systems such as blankets, thermal coatings, bare fixed in place http://news.bbc.co.uk/2/hi/uk_news/england/leicestershire/7
and heat is transferred through a natural process. Passive 453497.stm.
thermal control will be used in our satellite.
Testing will be performed to meet all launch provider
requirements as well as any additional requirements deemed
necessary to ensure the safety of the Cubesats. Comprehensive
test facility include thermal vacuum chamber and high power
shaker will be built, and LCRsat-I will undergo the random
vibration, thermal vacuum bake out, and shock tests.
. Conclusion
9. Others
Acknowledgments
References