179 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 179 total) Real-time optimal control of quadrocopters using deep representations of the optimal state feedback A major challenge in the field of control is to achieve reliable, aggressive, high-speed control of autonomous vehicles. In space, this may involve spacecraft that need to land under harsh conditions, or even – in an extreme scenario – negotiating asteroid debris fields at high speeds. On Earth, the exemplar task that draws most attention currently is high-speed autonomous flight of drones. The application of optimal control on board limited platforms has been severely hindered by the large computational requirements of current state-of-the-art implementations. The Netherlands Discovery 18-8510 TU DELFT 2018 - 2019 Real-time optimal control of quadrocopters using deep representations of the optimal state feedback De-risk assessment: ATENA-EGS-CC-compatible automation system for AIT/AIV and Operations based on OTX ATENA system is easy to access by many users and its maintence is effective. In addition, the system has a modern UX/UI which is developed as a web-based application. Within the ATENA we have a special set of building blocks enabling communication and test of equipment defined using SSM (Space System Model) concept. Within the de-risk we have also developed integration mechanisms that enables testing of prototype EGS-CC system connected with RTF Simulator. Poland GSTP G617-241TAbo ITTI SP. Z O.O. 2018 - 2019 De-risk assessment: ATENA-EGS-CC-compatible automation system for AIT/AIV and Operations based on OTX De-risk assessment: Queue commanding for navigation cameras The Max Planck Institute for Solar System Research (MPS) has developed and operated the imagining systems used for navigation and science in the Rosetta and Dawn missions. The objective of this project was to use recent lessons learned and competences acquired from these missions to develop a queue server and external commanding capability for future onboard image acquisition and image processing systems supporting advanced onboard autonomous navigation. Germany GSTP G617-241TAbq MAX PLANCK GESELLSCHAFT ZUR FOERDERUNG DER WISSENSCHAFTEN 2019 - 2019 De-risk assessment: Queue commanding for navigation cameras Real-time verification and testing facilities for image processing for navigation The facilities shall be suited for any space flight mission specially those relying on image processing for navigation (visible, infrared, multispectral, LIDAR). The facilities shall support MIL, SIL, PIL, and HIL verification types, and shall allow testing in open-loop and closed-loop configurations. Subsystem aspects shall be considered to cover interdisciplinary verification aspects. The facilities shall be modular, supporting fast and flexible scenario configuration and shall be movable and relocatable. Germany GSTP G617-282SA ASTOS SOLUTIONS GMBH 2017 - 2019 Real-time verification and testing facilities for image processing for navigation Deployment of PUS-C standard in projects supported by an automatic generation toolset Addressing the utilization of telecommand and telemetry packets for the purpose of remote monitoring and control of the spacecraft, the Packet Utilization Standard (PUS) is one of the few ECSS engineering standards that is applied from the development of the Spacecraft, subsystems and payloads but also in the development of the Ground Segment and to the Operations.Producing a new PUS that includes the last 10 years of lessons learned, the PUS Working Group has applied some formal requirement engineering techniques with as intended objective to enable the capability to automate the productio Belgium TDE T702-406SW SPACEBEL SA. 2016 - 2019 Deployment of PUS-C standard in projects supported by an automatic generation toolset De-risk assessment: Space Qualification and reference design for Myriad2 Video Processor Myriad is a commercial Computer Vision (CV) and Artificial Intelligence (AI) processor that is both high-performance and low power, operating in a nominal 1.5W power envelope. Its bottom-up design for edge compute makes it an attractive solution for on-board and in-flight data processing, where it can enable AI inference on CubeSats. Flying a COTS device for the first time requires several stages of test, design and development, and this activity supports multiples of these stages. Ireland GSTP G617-241TAaf Jaliko Ltd. 2018 - 2019 De-risk assessment: Space Qualification and reference design for Myriad2 Video Processor Qualification activity for COTS IMA Kernel In order to address the increasing complexity of spacecraft avionics, ESA is adopting a technological solution from the aviation domain: Integrated Modular Avionics (IMA). In the early 1990s, the aeronautical domain defined a solution which, by means of software partitioning, allows for integration of several functions onto the same computational node while still keeping them separated from each other in a way which also preserves many of the benefits of a federated systems approach. Germany GSTP G617-253SW EMBEDDED BRAINS GMBH 2018 - 2019 Qualification activity for COTS IMA Kernel Compact Reconfigurable Avionics : Reconfigurable Data Handling Core The general approach while designing a Reconfigurable Avionics will follow the general principles: - Implementing by default most of the functions as SW - Using (slave) reprogrammable FPGA(s) as an accelerator to implement too CPU intensive functions - Providing a scalable and versatile I/O system supported by flexible SW drivers - Extending digital I/Os by Analogue Front-ends The selected hardware platform is the combination of a powerful microprocessor and one or several high-end reconfigurable FPGAs, fulfilling the following needs: - Supporting exploratory and evolutionary designs accord Sweden TDE T701-504ED COBHAM GAISLER AB 2019 - 2019 Compact Reconfigurable Avionics : Reconfigurable Data Handling Core Proba-Next Avionics Architecture Definition and Design In the frame of the GSTP program, an activity called Advanced Data and Power Management System (ADPMS) was initiated in 2000. This activity had the objective to develop advanced combined power management and data handling in a single box targeting Proba like small platforms. The activity resulted in the complete design of the core of the Proba platform avionics and was produced in flight models for Proba-2 and Proba-V. Both satellites are now in orbit and are cumulating more than 5 years of operations. Belgium GSTP G617-159SY QINETIQ SPACE NV 2016 - 2019 Proba-Next Avionics Architecture Definition and Design Modelling of Spacewire Networks After more than 15 years of development at international level lead by ESA, SpaceWire has become the workhorse for high data rate on-board communications, not only for ESA missions but for other space agencies (NASA, JAXA, ROSCOSMOS) and for the space industry. This technology has become a de facto standard for payload systems and is now being used for avionics. The capability provided by SpaceWire to develop data handling systems based on high-speed networks rather than low-speed buses allows much greater performance but implies mastering much more complex communication schemes. 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