Antennas for CubeSat Communication

CubeSats are a type of small satellites (< 500 kg) that weigh several kilograms and consist of multiple Units (U) measuring 100 × 100 × 113.5 mm3. CubeSats emerged as a low-cost alternative to conventional large satellites, and have since demonstrated capabilities for communication, Earth observation, technology demonstration and many other. The primary goal of CubeSats, as it is the case with any miniaturized satellite, is to reduce the cost of orbital deployment. CubeSats are commonly launched as a secondary payload on large launch vehicles. One or several satellites are placed in a dedicated deployment system, which typically accommodates three CubeSat Units. The deployment system strictly limits the dimensions of any features on the CubeSat surface. CubeSat antennas perform the same functions as antennas on conventional satellites, such as telemetry and command, communication, navigation or inter-satellite links (ISL). However, most traditional antennas for small satellites are not suitable for CubeSats due to the profile constraints of the deployment system. Two approaches for antenna design are generally adopted. In the first, one or several low-profile antennas are placed on the CubeSat exterior. In the second, deployable antenna structures are used if the CubeSat platform does not offer sufficient dimensions. At low frequencies, the additional space is required to achieve a good radiation efficiency, whereas at high frequencies an increased antenna aperture provides a high gain. This thesis describes several antenna geometries, both low-profile and deployable, which enable several communication aspects of an Internet-of-Things (IoT) constellation of 3U CubeSats in the Low Earth Orbit (LEO). The main novelty of the proposed solutions is in their electromagnetic performance, as opposed to most CubeSat antenna designs where the mechanical design is the main achievement. The presented antennas succeed to exhibit a wide bandwidth or a specified radiation under strict size constraints. The thesis presents several wideband aperture-coupled patch antennas for TT&C and data downlink in S and X bands. A thoroughly investigated shielded-stripline feeding structure enables a wideband circular polarization (CP) with a unidirectional radiation, and demonstrates capabilities such as interference suppression of adjacent frequencies and efficient CubeSat integration. Patch-antenna arrays in L band are then presented, which radiate several independent beams for the capacity increase of an IoT machine-to-machine (M2M) communication system. The high permittivity of the antenna substrates lead to a strong coupling to the 3U CubeSat structure, emphasizing the importance of the antenna placement. Finally, different configurations of high-gain fixed-beam reflectarrays (RA) and transmitarrays (TA) are for the first time proposed for CubeSat ISL LEO communications in K band. Two novel unit cells are presented for RA and TA antennas, based on coupled loops and aperture-coupled patches, respectively. An axially corrugated CP horn antenna is designed as the feeding element for the arrays. A prototype of this antenna is fabricated using additive manufacturing in aluminum. The performance of all antennas, presented in this thesis, is validated by agreements between the calculation and 3D-simulation results and the VNA and anechoic-chamber measurements of several prototypes.

Design of novel radiating elements for SATCOM phased arrays in Ku-Band

Baptiste Fernand Hornecker

The present thesis deals with the design of a planar antenna array for the communication between a civil aircraft (Dassault's Falcon) and an Inmarsat satellite. The final goal is to provide high speed Internet access in X/Ku-Band (8-12GHz / 12-18GHz), and possibly even in K/Ka- Band (18-27GHz / 17-40GHz). The study starts with the Ku-Band only, then evolves towards the transmission band and finishes with their Ka-Band counterparts. The main constraint of the thesis is that the final result should be a low profile antenna that will be easy to integrate below the fuselage of an aircraft. At the same time, the antenna has to provide a beam steering mechanism in order to track the position of the targetted satellite while the aircraft is moving. The usual way to achieve it is to implement some dedicated electronic chips below each radiating element of array. Dassault Aviation has its own alternate and more mechanical oriented solutions. Since the communication system is intended for top-notch business jets produced in small series, cost is not here a decisive criterion. This thesis assumes the existence of the beam-steering system and concentrates on a proof of concept and careful design of the antenna elements that will constitute the final array. They have to satisfy tight constraints in terms of size, return loss, mutual coupling with neighbors, efficiency, radiation pattern and dual circular polarization quality. Printed multilayer antennas have been retained as the best candidates, and themain parts of the thesis have been dedicated to their study. The thesis concludes with the presentation of an apparently completely unrelated and independant topic, namely the simulation of nanoscale 2D planar structures based on Graphene. The rationale for this last chapter is to provide a prospective study of the use of Graphene to create a variable capacitance. This component is always needed in the beamforming network of reconfigurable and scanning arrays. Our laboratory is developing a deep knowledge of the electromagnetic properties of Graphene-based devices and these varicaps could lead to very interesting applications in high frequencies, once the Graphene technology has definitely progressed. Thanks to electrostatics Green's functions, a variable capacitor based on Graphene has been simulated, and a Quantumeffect -the Quantum capacitance of Graphene- has been successfully tackled from a numerical point of view.

EPFL2016

A simple & [and] accessible front-end satellite receiver for communications and e-learning in emerging countries

Olivier Videme Bossou

For the universities of the emergent countries, and those of Cameroon in particular, the fight to reach a durable development requires to know the needed scientific and technical information for their development, how to get it and to spread it out among partners in the country. Obviously, the complete answer to these preoccupations lies well beyond the framework of this project, but a projection, partial but highly significant, can nevertheless be obtained if one concentrates one's efforts on a specific technological field : in the present study, we shall treat of antennas for telecommunications systems. This subject is highly suitable as example and potential incubator for future achievements. The ultimate goal is to design and carry out the fabrication of a system of satellite communications adapted to the financial resources and to the development needs of the universities of the South. First of all, we will review the state of the art in satellite communication systems, both for already operating ones and also for new systems, still under development. Then we will determine which system of satellite telecommunications has a receiver and communication fees with affordable costs : our choice will be made on Worldspace satellite system, which was actually designed for developing countries. We will also review the status of planar antenna and low noise amplifier technology, and then explicit the basic challenge involved in our thesis project. One of the aims of this project is to use local wood as dielectric in SSFIP type antennas. Before using a material as dielectric in an antenna design, it must be characterized. Before carrying the characterization of local wood species, we will begin by reviewing some commonly used dielectric measurement techniques. Then we will carry out a series of measurements to characterize the species of wood growing in the Cameroonian forest. At the end of the series of measurements and according to the dielectric losses observed, we will select the species of wood best suited to make a good substrate for a microstrip antenna. Next, we will design, manufacture and test low cost antennas. These antennas must satisfy not only technical criteria compatible with those of the telecommunications system chosen but, even most importantly, it must meet socioeconomic criteria : the antennas must be manufactured with low cost and locally available materials, making use of simple technological processes. Once we have found the wood species that exhibits the lowest dielectric losses, we will simulate, and then manufacture the SSFIP type antenna with wood as substrate and aluminium as conducting element. Then we will measure its characteristics and check whether they are compatible with those of a Worldspace receiver. The signal received from the satellite by the antenna is very weak. It will be important to strengthen the received signal with a low noise amplifier (LNA) before connecting the antenna to the receiver. Thus the antenna and the LNA constitute an active antenna and form what we call here the radiofrequency (RF) front-end. We will design, manufacture and measure the LNA characteristics. A simple manufacturing process must be used to realize these antennas, because later on they must be manufactured locally in Cameroon : this is a determining challenge to ensure the economic independence, which is essential in our thesis project. Afterwards we will join the LNA to the planar antenna and connect the active antenna obtained in this manner to a commercial Worldspace receiver. Finally, we will perform receiving tests of the Worldspace radio station with the system designed. In parallel, our project includes a second goal, which presents an equivalent significance. We will use existing Matlab codes to develop an online course to teach antenna theory. In addition, at the end of the project and when the Cameroonian local manufacture would have started, we will put all algorithms used for the antenna design on the web site in a multi-media applet, together with a complete documentation of all the manufacturing technologies used. The courses that already exist in Lausanne and Yaounde, relating to the description of other types of antennas will be added, thus leading to a complete teachware that would ensure the durability and the dissemination of the results obtained, and would provide an invaluable tool for teaching and training.

EPFL2007

Aperture-Coupled Low-Profile Wideband Patch Antennas for CubeSat

Anja Skrivervik Favre, Miroslav Veljovic

This communication presents the design and measurement results of aperture-coupled stripline-fed wideband patch antennas for nanosatellite applications. The low-profile requirements lead to a strong back radiation from the coupling aperture. Instead of suppressing the resulting electric field in the feeding stripline, an advantageous field distribution is used to boost the electromagnetic coupling to the radiating element. This effect is achieved by enclosing the stripline feeding structure with vertical conductive walls, effectively creating a cavity. The obtained antenna has a low profile of 0.08 lambda 0 at 2 GHz and exhibits 3 dB gain and axial ratio bandwidths of 27% and 32%, respectively. The effect of cavity resonances is analyzed in detail and we show how it is used to reduce the interference in adjacent frequency bands. This communication also proposes an elegant method of integrating this type of antennas into the satellite chassis, which reduces the antenna extrusion on the satellite surface. The two proposed methods are demonstrated through another antenna prototype mounted on a low-cost CubeSat mock-up.