Skip to main content
BlackBridge owns and operates the RapidEye remote sensing constellation. The 5 satellites are capable of imaging more than 5 million square kilometres a day in 5 spectral bands. The tasking algorithm of the satellites is based on a tile... more
BlackBridge owns and operates the RapidEye remote sensing constellation. The 5 satellites are capable of imaging more than 5 million square kilometres a day in 5 spectral bands. The tasking algorithm of the satellites is based on a tile score system that accounts for the constraint that the RapidEye satellites were not designed to perform roll maneuvers between image takes on the same orbit. A more agile attitude control system, featuring the capability of performing roll maneuvers between individual image takes can further optimize the image collection. This paper shows that such a system grants the tasking process a larger flexibility and enables a faster coverage of the areas of interest. It depicts the impact of the attitude control system agility on the acquisition capacity of remote sensing constellations. Statistical cloud data is used to reproduce the tasking process and to simulate three imaging campaigns of large areas. The paper shows the acquisition capacity of the agile...
There are various robotic On-Orbit Servicing concepts existing, which aim at utilizing inspector satellites for obtaining high-fidelity video feedback from the remote environment. Most of these inspection tasks, which involve proximity... more
There are various robotic On-Orbit Servicing concepts existing, which aim at utilizing inspector satellites for obtaining high-fidelity video feedback from the remote environment. Most of these inspection tasks, which involve proximity operations, can be done autonomously by the spacecraft. However, there are cases such as sensor malfunctions or undefined spacecraft states, in which it seems advantageous to have the possibility of human interaction with the inspector satellite. An operator on ground with the capability of real-time control can complement autonomous operations and add robustness to mission operations. The SPHERES Interact program at the MIT Space Systems Laboratory currently develops concepts for efficient human spacecraft interaction. Using three experimental satellites aboard the International Space Station, a series of tests were executed, which evaluated different approaches and methods. Additionally, using another three of these experimental satellites on the air bearing table at the Space Systems Laboratory, advanced concepts can already be developed and verified on ground. This paper shows experiments, in which the SPHERES at MIT were controlled via a geostationary relay satellite of the European Space Agency (ESA), using a ground station in Germany. It emphasizes the benefits of real-time human spacecraft interaction and describes the design of the associated test environment.
... Enrico Stoll, Alvar Saenz-Otero, and Brent Tweddle ... The main objective of the SPHERES Goggles is to provide a flight-traceable platform for the development, testing and maturation of computer vision-based navigation algorithms for... more
... Enrico Stoll, Alvar Saenz-Otero, and Brent Tweddle ... The main objective of the SPHERES Goggles is to provide a flight-traceable platform for the development, testing and maturation of computer vision-based navigation algorithms for space-craft proximity operations. ...
In this paper we present the realization of a test environment to test preflight high-fidelity inter-satellite communication links on ground. The basic requirements are given by the research project “Telepresence for Space Missions” as... more
In this paper we present the realization of a test environment to test preflight high-fidelity inter-satellite communication links on ground. The basic requirements are given by the research project “Telepresence for Space Missions” as part of a collaborative research centre (SFB 453) funded by the German Research Community (DFG). The intention of this project is establishing a communication link from Low Earth Orbit (LEO) to a geostationary relay satellite in order to control robotic applications on LEO satellites. While about 0.6 seconds. To establish an Inter Satellite Link (ISL) a tracking mechanism for a steerable antenna is needed. To verify the functionality of the tracking mechanism, a test bed has been developed at the Institute of Astronautics using an existing concept of a test bed for an attitude simulation system. This test bed for attitude simulations is based on an antenna turntable which is part of the S-band ground station at the Institute of Astronautics. Using thi...
The vision1 of a space robot as an extended arm of the human operator on ground is a key component for onorbit robotic service missions. This concept of telepresence requires a high-quality sensor feedback from the space environment to... more
The vision1 of a space robot as an extended arm of the human operator on ground is a key component for onorbit robotic service missions. This concept of telepresence requires a high-quality sensor feedback from the space environment to the operator including stereo video and force-feedback. For the force feedback channel the knowledge of the signal delay time during operation is an important factor to increase the immersiveness of the system. In case of radio contact to space segments which are not in GEO, the signal delay time varies according to the distance between the spacecraft and the ground station. This paper proposes a method for deriving the required signal delay from the Doppler frequency shift alone which is readily available from the receiver since the actual signal delay is an input value for the control loop in the haptic channel.
In this paper we present a test environment to test preflight high-fidelity intersatellite communication links on ground. The basic requirements are given by the research project “Telepresence for Space Missions” which is part of a... more
In this paper we present a test environment to test preflight high-fidelity intersatellite communication links on ground. The basic requirements are given by the research project “Telepresence for Space Missions” which is part of a collaborative research centre (SFB 453 – Sonderforschungsbereich) funded by the Deutsche Forschungsgemeinschaft (DFG). The goal of this project is to analyze and test the possibility of establishing a communication link via a geostationary relay satellite having a signal roundtrip time smaller than 0.8 seconds. To establish a link between a Low Earth Orbit (LEO) satellite and a geostationary relay satellite, an Inter Satellite Link (ISL) tracking mechanism to steer the antenna is needed. To verify the functionality of the tracking mechanism, a test bed similar to attitude control system test beds had to be developed at the Institute of Astronautics. Start-ing from the requirements of the attitude control system for an on-orbit servicing mission, a selecti...
Within the last three years, the Joint Space Operations Center (JSpOC) detected 85 close approaches between the RapidEye constellation and secondary space objects. Most of the approaching objects were non-operational, such as debris from... more
Within the last three years, the Joint Space Operations Center (JSpOC) detected 85 close approaches between the RapidEye constellation and secondary space objects. Most of the approaching objects were non-operational, such as debris from the Chinese Fengyun 1C satellite.
An Inter-Satellite Link Antenna (LISA), developed for transmitting data via a geostationary relay satellites is attached to a three degree of freedom satellite attitude simulator in order to validate not only the pointing mechanism of the... more
An Inter-Satellite Link Antenna (LISA), developed for transmitting data via a geostationary relay satellites is attached to a three degree of freedom satellite attitude simulator in order to validate not only the pointing mechanism of the antenna but also the algorithms on-ground. While the device is simulating a satellite orbiting in LEO the antenna will compensate the rotational motions and maintain a link to the ESA relay satellite ARTEMIS. This paper gives an overview on the efforts that have be undertaken to use real satellite data for testing the link maintenance of the inter satellite link antenna on-ground. For reproducing satellite attitude by means of a simulator with 3 rotational degrees of freedom an inter-satellite link based coordinate frame is not only introduced at the orbiting satellite and but also at the satellite on the simulator on-ground. This coordinate frame and related Euler angle conversions are the basis for obtaining angular data which is essential for th...
A test bed for telepresent space applications that utilizes geostationary satellites for data relay has been developed at the Institute of Astronautics. The research focus is on the verification of a newly developed Light-weight Inter... more
A test bed for telepresent space applications that utilizes geostationary satellites for data relay has been developed at the Institute of Astronautics. The research focus is on the verification of a newly developed Light-weight Inter Satellite Link Antenna (LISA) for small satellites, and the corresponding steering mechanism and pointing algorithm. For inter-satellite links to the ESA relay satellite ARTEMIS link properties, signal round trip times, and the applicability of CCSDS protocols are investigated. For the test environment, an existing ground station has been modified and connected to a satellite attitude simulator. A first test scenario involving bilateral telecontrol is described.
The research activities of the Institute of Astronautics (IA) are focused on the analysis of the communication scenario of robotic space missions in detail. That includes also verification of a newly developed Light-weight Inter Satellite... more
The research activities of the Institute of Astronautics (IA) are focused on the analysis of the communication scenario of robotic space missions in detail. That includes also verification of a newly developed Light-weight Inter Satellite Link Antenna (LISA) for small satellites, corresponding steering mechanism and pointing algorithm. The investigation of inter-satellite links is mainly focused on transparent relay satellites which allow data relay between low earth orbit (LEO) and geostationary orbit (GEO) satellites. Therefore the ESA satellite ARTEMIS stands in the main focus of the research work of the Institute. The most important requirement for robotic space missions is given by the time delay between the operator on earth and the manipulator in space. Data processing and data handling strategies are playing also a important role in robotic space mission and are under investigation. The Institute of Astronautics realized a special test environment to investigate these points...
Spacecrafts are the only complex engineering systems without hands-on maintenance and repair-supporting infrastructure. Though occasionally there have been Space-Shuttle-based servicing missions, such as the Solar Maximum Repair Mission... more
Spacecrafts are the only complex engineering systems without hands-on maintenance and repair-supporting infrastructure. Though occasionally there have been Space-Shuttle-based servicing missions, such as the Solar Maximum Repair Mission (SMRM) in 1984, usually on-orbit mainten-ance procedures are not foreseen for an individual spacecraft. However, the explorative and manipulative possibilities of robots could be used to dock a ser-vicer spacecraft onto a malfunctioning target spacecraft and execute On-Orbit Servicing (OOS) operations, controlled by an operator from ground. To date the servicing spacecrafts of most of the robotic OOS demonstration missions are equipped with a high degree of autonomy. A differ-ent approach is to utilize the concept of telepresence for OOS. It involves the permanent control of the servicer satellite and its robotic components from ground. This paper describes a test environment for telepresent OOS, which included the ground station of the Institute of ...
The authority over search and rescue operations (SAR) rests to the so-called rescue coordination center in the Federal Republic of Germany. An essential element for the coordination of SAR operations in general is the communication... more
The authority over search and rescue operations (SAR) rests to the so-called rescue coordination center in the Federal Republic of Germany. An essential element for the coordination of SAR operations in general is the communication between rescue workers and the rescue coordination center. A detailed description of the situation at a remote place, given by the incoming rescue teams, allows the rescue coordination center to get an overview of the scene and to make timely decisions regarding the necessity of a second alarm or calling special forces to the scene. A satellite based extension of the communication chain to, that enables video feedback the rescue coordination center fromon the remote site is a core element of this paper. This extension is realized using a satellite controlled multi-sensor unmanned aerial vehicle (UAV). A radio controlled copter is used that permits telepresent operations and thus, enables the rescue control center to initiate autonomous procedures at the s...
ABSTRACT This paper will show how the combination of the software tools MDVE (Model-based Development and Verification Environment) and Framtec (Framework for advanced Moni-toring, Telemetry and Control) as used in the BayernSat project... more
ABSTRACT This paper will show how the combination of the software tools MDVE (Model-based Development and Verification Environment) and Framtec (Framework for advanced Moni-toring, Telemetry and Control) as used in the BayernSat project will support meeting these two requirements. The software tool MDVE is an environment for developing, modeling, simulating and verifying satellite systems, which allows for a fully simulated satellite and a step by step hardware in the loop implementation of the satellite. The Monitoring & Control tool Framtec will be configured during the development process and will be used in its final configuration for BayernSat TMTC. The combination of these software tools allows a pre-optimization of the data signal delay time in the early development phase. Therefore, it is possible to get a first estimation and verification of the implemented data structure on ground and in space prior to the mission operation phase.
Collision avoidance is a topic of increasing importance. The number of satellites in Earth orbit is steadily growing and with the high amount of space debris, either crossing through or resident in orbit, collision probabilities between... more
Collision avoidance is a topic of increasing importance. The number of satellites in Earth orbit is steadily growing and with the high amount of space debris, either crossing through or resident in orbit, collision probabilities between two such objects can become critical. Small satellite missions usually operate with limited capabilities when it comes to locating potential collision occurrences and deriving the associated collision probability. Accordingly, they have to rely on external organizations, such as the Joint Space Operation Center (JSpOC) and their information system to plan for contingency operations. This paper reviews the benefits of using such an external service for a small satellite constellation. It analyses the relevant data for use in daily operations and shows collision avoidance approaches based on the available data. Conjunction summaries for the RapidEye satellite constellation are evaluated and their influence on the planning of collision avoidance maneuve...
This paper describes the concept for an End-to-End test environment using the developed Ka-Band inter-satellite antenna in combination with the Ka-band mock-up system of the Institute of Astronautics (LRT – Lehrstuhl Raumfahrttechnik) at... more
This paper describes the concept for an End-to-End test environment using the developed Ka-Band inter-satellite antenna in combination with the Ka-band mock-up system of the Institute of Astronautics (LRT – Lehrstuhl Raumfahrttechnik) at Technische Universitaet Muenchen. As the Ka-Band mock-up is an outdoor 3-axis attitude simulator facility, the paper further outlines the major aspects, which had to be taken into account with respect to the communication link calculation (atmospheric influence, spot pattern reconstruction, gain variations etc.) and attitude control of the servicer satellite and the relay satellite, like attitude biasing.
ABSTRACT This paper shows how to reduce cost und configuration time by using FRAMTEC as a Monitoring and Control tool in mission operation phase as used in the satellite project “BayernSat” of the Institute of Astronautics / Technische... more
ABSTRACT This paper shows how to reduce cost und configuration time by using FRAMTEC as a Monitoring and Control tool in mission operation phase as used in the satellite project “BayernSat” of the Institute of Astronautics / Technische Universität München. The employment of Framtec as a M&C tool for the whole Electrical Ground Support Equipment – EGSE allows the continuous configuration over during the development phases of a satellite. This integration of the software tool FRAMTEC in the development process and phases and its benefit in cost- and time-efficient is described. Finally, an outlook in realizing this approach is discussed.
ABSTRACT Upcoming space missions utilizing hyperspectral or other high-resolution sensors will generate a vast amount of data in orbit. The average communication duration between a spacecraft in low Earth orbit (LEO) to a dedicated ground... more
ABSTRACT Upcoming space missions utilizing hyperspectral or other high-resolution sensors will generate a vast amount of data in orbit. The average communication duration between a spacecraft in low Earth orbit (LEO) to a dedicated ground station is short and in addition, due to the high amount of data to be transferred at link times, a high-performance communication system on board of the satellite is indispensable.A solution that provides longer acquisition times with the ground station is to employ a high data-rate inter-satellite link to a geostationary relay satellite, which requires a flat, compact, steerable, light-weight yet robust antenna. Such an antenna system (antenna module plus pointing module) was developed for S-Band at the Institute of Astronautics (Technische Universität München), in cooperation with German space companies, research institutes and the German Aerospace Center (DLR). Its successful operation via the geostationary relay satellite Artemis was demonstrated in cooperation with ESA in 2007.This paper describes the evaluation of an antenna system in the Ka-Band, as a successor to be developed in the next two years for high data rates and the various applications of such an antenna system.
RapidEye is a commercial remote sensing mission delivering geospatial information. Five identical satellites in a sun-synchronous orbit image more than four million square kilometers per day. RapidEye features the unique ability to... more
RapidEye is a commercial remote sensing mission delivering geospatial information. Five identical satellites in a sun-synchronous orbit image more than four million square kilometers per day. RapidEye features the unique ability to revisit any area on Earth daily. Within three years of operation, the constellation mastered a number of complex challenges, which led to an evolved mission concept. RapidEye started