A Cost-Effective Ground Station for Small Satellite Operations

2019 ◽  
Vol 2019 ◽  
pp. 1-13 ◽  
Author(s):  
Yan-Jie Song ◽  
Zhong-Shan Zhang ◽  
Kai Sun ◽  
Feng Yao ◽  
Ying-Wu Chen

Small satellite image downlink scheduling problem (SSIDSP) is an important part of satellite mission planning. SSIDSP mainly needs to balance how to better match the limited receiving capacity of the ground station with the limited satellite resources. In this paper, regional targets are considered with SSIDSP. We propose a mathematical model that maximizes profit by considering time value and regional targets. A downlink schedule algorithm (DSA) is proposed to complete the task sequence arrangement and generate scheduling results. A heuristic genetic algorithm (HGA) is used to optimize the generated task sequence to achieve higher profit. Three scale test instances are used to test the effectiveness of HGA and DSA. We compare the effect of HGA, basic genetic algorithm (GA), and construction heuristic algorithm. The experimental results proved that the proposed approach ensures the successful completion of observation tasks and is effective for SSIDSP.


Author(s):  
Fred V. Brock ◽  
Scott J. Richardson

Measurements of atmospheric properties become progressively more difficult with altitude above the surface of the earth, and even surface measurements are difficult over the oceans. First balloons, then airplanes and rockets, were used to carry instruments aloft to make in-situ measurements. Now remote sensors, both ground-based and satellite-borne, are used to monitor the atmosphere. In this context, upper air means all of the troposphere above the first hundred meters or so and, in some cases, the stratosphere. There are many uncertainties associated with remote sensing, so there is a demand for in-situ sensors to verify remote measurements. In addition, the balloon- borne instrument package is relatively inexpensive. However, it should be noted that cost is a matter of perspective; a satellite with its instrumentation, ground station, etc. may be cost-effective when the mission is to make measurements all over the world with good space and time resolution, as synoptic meteorology demands. Upper air measurements of pressure, temperature, water vapor, and winds can be made using in-situ instrument packages (carried aloft by balloons, rockets, or airplanes) and by remote sensors. Remote sensors can be classified as active (energy emitters like radar or lidar) or passive (receiving only, like microwave radiometers), and by whether they “look” up from the ground or down from a satellite. Remote sensors are surveyed briefly before discussing in-situ instruments. Profiles of temperature, humidity, density, etc. can be estimated from satellites using multiple narrow-band radiometers. These are passive sensors that measure longwave radiation upwelling from the atmosphere. For example, temperature profiles can be estimated from satellites by measuring infrared radiation emitted by CO2 (bands around 5000 μm) and O2 (bands around 3.4μm and 15μm) in the atmosphere. Winds can be estimated from cloud movements or by using the Doppler frequency shift due to some component of the atmosphere being carried along with the wind. An active sensor (radar) is used to estimate precipitation and, if it is a Doppler radar, determine winds. The great advantage of satellite-borne instruments is that they can cover the whole earth with excellent spatial resolution.


2021 ◽  
Author(s):  
G. Governale ◽  
J. Rimani ◽  
N. Viola ◽  
V. Fernandez Villace

AbstractThe trend of cost-effective access to space and satellite technologies’ evolution is increasing the small satellite market. However, small payloads usually ride as piggyback, being a secondary passenger of a space vector, with very low flexibility in target orbit and launch schedule. The micro-launchers are designed to answer the needs of the small satellite missions, with a payload capacity up to 350 kg to Low Earth Orbit, aiming to low turn-over time and competitive prices. This paper explains the work performed by Politecnico di Torino in support of the ESA–ESTEC activities on micro-launchers. The aim is to provide preliminary guidelines for choosing and evaluating new innovative micro-launcher flight vehicle engineering processes. A trade-off methodology is proposed and defined based on the Analytically Hierarchical Process (AHP). This methodology considers, among other features, the flight profile, maximum payload, and physical characteristics. To support the trade-off analysis, a software tool is built for the automatic generation of the aerodynamics and propulsion parameters needed for the completion of the preliminary designs, enabling the performance estimation. The launcher’s performance models, with an analysis of the take-off sites and target orbits, are also produced. This allows the definition of performance maps where the maximum payload is graphed as a function of the orbit altitude and inclination. A set of innovative micro-launchers exploiting different technologies is also assessed as a case study.


2014 ◽  
Vol 875-877 ◽  
pp. 2092-2096
Author(s):  
Chafaa Hamrouni ◽  
Bilel Neji ◽  
Adel M. Alimi

Pico Satellite Telecommunication with Ground Station (GS) is Characterized by a Limitedline of Sight that Affects Transmission Delay and Data. in this Paper, a New Fuzzy Logic Control Systemmodel is Proposed to Ensure a Long Lasting Ground Station (G.S) Visibility to Pico Satellite Duringorbiting in Leo. Developed System is Helpful to Control Wave Propagation for Transmission. Presentedmethod Describes a Fuzzy Switching Control System for both Side Microstrip Antennas Array Systemmodel that Guarantee a Maximum Transmission Time and Achieves Small Satellite Communicationcontrol Performance with Simplified Control Scheme. the Method Includes Switched Systemmodeling, Fuzzy Control System Design, and Optimized Fuzzy Modeling Algorithm; in Addition Petri Netmodeling is Developed to Predict System Behavior. Added Algorithms were Simulated and Tested.Proposed System and Integrated Algorithms Performance were Demonstrated in the Reportedsimulations and Tests Results.


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