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Flight Dynamics System Software Engineering

2016-03-10 19:08:52| Space-careers.com Jobs RSS

With 1.700 employees worldwide, the CS Group is a leading IT company in France and in Germany, and a prime contractor in designing, integrating and operating mission critical systems. It has now been over 30 years that comprehensive CS solutions for space systems and applications, both on the ground and in space, have been part and parcel of this odyssey. Our German activities grow at fast pace and to face our costumers high level expectations and needs, we are looking for talented profiles having relevant experience in Space systems. This job position is for our customer EUMETSAT. The key person will work in the TSS Department as a member of the Mission Control Applications and Tools Team, which is part of the GSI Division. The key person will provide hisher prime support to the Mission Control Applications and Tools Team and heshe will support the evolution and maintenance of the EUMETSA T Flight Dynamics Systems for LEO missions. the requirements specification, design, implementation, integration and verification of Flight Dynamics Systems for new EUMETSAT LEO Programmes PhaseBCD, including the setting up of the related maintenance arrangements and processes. the technical coordination in the team of the different parallel activities involving the EUMETSAT Flight Dynamics Systems for LEO missions. The tasks of the key person will typically include Maintenance and Evolution Activities Reengineering activities analysis of the porting of some subsystems to stateoftheart technologies, tradeoff studies of various technologies, software design of the technical solutions, following the procurement of the changes with external contractors and verification testing of the changes. Evolutions and changes generation andor analysis of userdriven and maintenance driven software requirements, software design of the technical solutions, following the procurement of the changes with external contractors and verification testing of the changes. Preventive and corrective maintenance including the investigation and correction or following the corrections implemented by external contractors of anomalies in the software facilities and verification testing of the fixes. Maintenance test procedures generation and updates of maintenance test procedures at software facility level and at system level. Support and development of the verification infrastructure development andor procurement of scripts I tools to perform installation checks, nonregression, functional and performance testing. Analysis and implementation of mechanisms or tools allowing the automatic or semiautomatic verification testing of the application software. Coordination of the production of new software releases or patches, delivevry acceptance and installation onsite. This activity includes the technical coordination of the production by an external contractor of new releases or patches of the application software, liaison with the EUMETSAT operational users, participation in technical reviews, participation in factory at contractor premises acceptance testing campaigns and coordination of the installation of the releases or patches onsite at EUMETSAT. Execution and coordination of software verification and nonregression testing campaigns. This activity includes preparation of test data, running the test procedures on the target system, generation of test reports, analysis of results and troubleshooting of problems. Software support software support to the endusers of the application software. Ensure operations continuity by provision of oncall services and software support to operations. Documentation generation and updates of technical documents. Technical point of contact for maintenance contractors acting as point of contact with the contractor for technical discussions, review of technical documentation from the contractor, organizing periodical technical meetings with the contractor. Support to new Missions PhaseB activities Requirements engineering Participation in the functional analysis and decomposition of the Ground Segment requirements in the domain of Flight Dynamics System. Support the definition of Ground Segment requirements in the area of the Flight Dynamics System. Participation in workshops and review meetings. Interfacing with Operations to consolidate the operational concept in the Flight Dynamics System requirements. Support the identification of the verification method and initial test cases for the Flight Dynamics System requirements. Incorporate the reuse of the EUMETSA T Flight Dynamics System kernel products in the Ground Segment requirements. Interfacing with the Flight Dynamics System kernel product experts in the MCA Team to coordinate their contributions to the requirements definition. Support to new Missions PhaseB activities System Architectural design Support the generation of the architectural system level design of the Flight Dynamics System as part of the Ground Segment. Support the production of design models using Systems Engineering and CASE tools. Support the definition and documentation of all interfaces IRDsICDs between the elements of the Flight Dynamics System and other Ground Segment or external elements. Incorporate the reuse of the EUMETSAT Flight Dynamics System kernel products in the Ground Segment design. Support to new Missions PhaseCD activities Support to Flight Dynamics System implementation Support to the requirement and design engineering activities as part of the applications development. Participation and contribution in requirements, design and implementation reviews both internal and with external contractors. Follow the software development by external contractors of the Flight Dynamics System. Support to new Missions PhaseCD activities Support to IV V and Acceptance Participation in verification readiness reviews and verification testing campaigns both internal and with external contractors. Technical coordination of the parallel activities involving the EUMETSAT Flight Dynamics Systems for LEO missions Support to the technical coordination of all the activities in the team where the EUMETSAT LEO Flight Dynamics Systems are involved. These activities comprise at the moment the maintenance and evolution for missions under routine operations, reengineering activities and the reuse of the EUMETSAT Flight Dynamics System in new Programmes. PROFILE In addition to having a University degree in a relevant engineering discipline, the key person shall demonstrate significant knowledge and experience in the area of specification, design, implementation, verification and maintenance of Flight Dynamics Systems. The key person shall have skills and experience in the following mandatory areas 1. Domain Skills Knowledge of the analytical principles for orbit determination and control of LEO spacecraft. Experience minimum 5 years in the definition of software requirements, architectural design, implementation and maintenance of Satellite Flight Dynamics Systems in the context of LEO missions based on the ESAIESOC NAPEOS Navigation Package for Earth Observation Satellite. 2. Software Development, Verification Maintenance Skills Experience minimum 5 years in the full cycle of development and maintenance of application software, preferably for Satellite Flight Dynamics Systems, following formal software engineering processes. This includes user and system requirement analysis, software requirement engineering, software design, implementation, corrective and evolutive maintenance activities. Experience minimum 3 years in IV V integration, verification and validation activities for Flight Dynamics Systems following formal engineering processes. This includes requirement verification, system and subsystem integration, generation of test plan and test procedures, nonregression testing, generation of test data, generation of test tools, running the test procedures on the target system, generation of test reports and anomaly tracking. 3. Software Engineering Skills Experience minimum 3 years in designing and developing software components and applications using Object Oriented 00 approach including design patterns. Experience minimum 3 years in designing and developing software applications using Java and related technologies. It would be a distinct advantage for the key person to have knowledge andor experience with some of the following 4. Domain Skills Experience with software development and maintenance of Tools using the Orekit space dynamics library. Experience in integration of Flight Dynamics Systems with Mission Control Systems based on MICONYS software suite from ESAESOC. Experience in integration of Flight Dynamics Systems with Mission Planning Systems. Experience with support to operations for Satellite Flight Dynamics Systems. 5. System Maintenance Skills Experience in being the technical point of contact for contractors working at offsite premises and responsible for application software evolution and maintenance. 6. Software Technology Skills IBM DOORS requirement management Tool. Experience in the usage of software CASE design tools e.g. Enterprise Architect andor MagicDraw. Experience in developing software applications using interfaces to relational database management systems RDBMS and experience with data model design for RDBMS. Unified Modelling Language UML for software design. Linux Operating System. XML processing schema design, validation, parser libraries, transformation XSLT andXPath. Experience in designing, developing and maintaining software client applications using Eclipse as HMI framework Rich Client Platform. Experience in designing and developing component based software applications using formal techniques e.g. OSGi. Experience using tools for the automation of software testing. The official languages of EUMETSAT are English and French. The working language for the position is English and therefore the Engineer must be able to work effectively in this language and have knowledge of the other. How to apply Please consider the following points before applying Please submit your complete application documents in English. An attached cover letter should mention your availability and salary expectations. Interested applicants should submit their CV to pierre.lenahediccssytems.de and copy to francoisxavier.laffontcs.fr with the job title. Due to new work permit restrictions for this position, please apply only if you are citizen of a European Union state or if you hold all appropriate documentation and permits to work in Europe. Closing date 18th April 2016 Starting Date 16th August 2016 Interviews week 1617 2016

Tags: system software engineering flight

 

Software, hardware short takes

2016-03-10 12:06:42| Oil IT Journal - www.oilit.com

IBM, Ansys, Allegro, Esri, CGG GeoConsulting, Energy Solutions, Kappa Engineering, Lasser, MicroSeismic, Midland Valley, Nutech, P97 Networks, Paradigm, Pegasus Vertex, Quorum, Read, Siemens.

Tags: software short hardware takes

 
 

2H Offshore Launches New Fracture Mechanics Software, FlawIQ

2016-03-10 01:52:22| oilandgasonline Home Page

2H Offshore, an Acteon company, has designed and launched a newEngineering Critical Assessment (ECA) software: FlawIQ.

Tags: software mechanics launches offshore

 

2H Offshore unveils new software for fatigue assessments of offshore components

2016-03-10 01:00:00| Offshore Technology

UK-based Acteon Group subsidiary 2H Offshore has launched its new software 'FlawIQ', which helps perform accurate fatigue assessments for offshore components.

Tags: of software components assessments

 

Flight Dynamics System Software Engineer

2016-03-09 22:06:50| Space-careers.com Jobs RSS

We are looking to further enhance our team by Flight Dynamics System Software Engineer You will be based initially for 2 years at our clients headquarters in Darmstadt, Germany. Extension of a further 2 years may be possible. In this large European Agency you will find an excellent and modern working environment with challenging tasks and responsibilities. Your Tasks Include The key person will provide hisher prime support to the Mission Control Applications and Tools Team and heshe will support The evolution and maintenance of the Flight Dynamics Systems for LEO missions. The requirements specification, design, implementation, integration and verification of Flight Dynamics Systems for new LEO Programmes PhaseBCD, including the setting up of the related maintenance arrangements and processes. The technical coordination in the team of the different parallel activities involving the Flight Dynamics Systems for LEO missions. The tasks of the key person will typically include Maintenance and Evolution Activities Reengineering activities analysis of the porting of some subsystems to stateoftheart technologies, tradeoff studies of various technologies, software design of the technical solutions, following the procurement of the changes with external contractors and verification testing of the changes. Evolutions and changes generation andor analysis of userdriven and maintenance driven software requirements, software design of the technical solutions, following the procurement of the changes with external contractors and verification testing of the changes. Preventive and corrective maintenance including the investigation and correction or following the corrections implemented by external contractors of anomalies in the software facilities and verification testing of the fixes. Maintenance test procedures generation and updates of maintenance test procedures at software facility level and at system level. Support and development of the verification infrastructure development andor procurement of scripts I tools to perform installation checks, nonregression, functional and performance testing. Analysis and implementation of mechanisms or tools allowing the automatic or semiautomatic verification testing of the application software. Coordination of the production of new software releases or patches, delivery acceptance and installation onsite This activity includes the technical coordination the production by an external contractor of new releases or patches of the application software, liaison with the Client operational users, participation in technical reviews, participation in factory at contractor premises acceptance testing campaigns and coordination of the installation of the releases or patches onsite. Execution and coordination of software verification and nonregression testing campaigns This activity includes preparation of test data, running the test procedures on the target system, generation of test reports, analysis of results and troubleshooting of problems. Software support software support to the endusers of the application software. Ensure operations continuity by provision of oncall services and software support to operations. Documentation generation and updates of technical documents. Technical point of contact for maintenance contractors acting as point of contact with the contractor for technical discussions, review of technical documentation from the contractor, organizing periodical technical meetings with the contractor. Support to new Missions PhaseB activities Requirements engineering Participation in the functional analysis and decomposition of the Ground Segment requirements in the domain of Flight Dynamics System. Support the definition of Ground Segment requirements in the area of the Flight Dynamics System. Participation in workshops and review meetings. Interfacing with Operations to consolidate the operational concept in the Flight Dynamics System requirements. Support the identification of the verification method and initial test cases for the Flight Dynamics System requirements. Incorporate the reuse of the Client Flight Dynamics System kernel products in the Ground Segment requirements. Interfacing with the Flight Dynamics System kernel product experts in the MCA Team to coordinate their contributions to the requirements definition. System Architectural design Support the generation of the architectural system level design of the Flight Dynamics System as part of the Ground Segment. Support the production of design models using Systems Engineering and CASE tools. Support the definition and documentation of all interfaces IRDsICDs between the elements of the Flight Dynamics System and other Ground Segment or external elements. Incorporate the reuse of the Clients Flight Dynamics System kernel products in the Ground Segment design. Support to new Missions PhaseCD activities Support to Flight Dynamics System implementation Support to the requirement and design engineering activities as part of the applications development. Participation and contribution in requirements, design and implementation reviews both internal and with external contractors. Follow the software development by external contractors of the Flight Dynamics System. Support to IV V and Acceptance Participation in verification readiness reviews and verification testing campaigns both internal and with external contractors. Technical coordination of the parallel activities involving the Flight Dynamics Systems for LEO missions Support to the technical coordination of all the activities in the team where the Clients LEO Flight Dynamics Systems are involved. These activities comprise at the moment the maintenance and evolution for missions under routine operations, reengineering activities and the reuse of the Clients Flight Dynamics System in new Programmes. Your Profile In addition to having a University degree in a relevant engineering discipline, the key person shall demonstrate significant knowledge and experience in the area of specification, design, implementation, verification and maintenance of Flight Dynamics Systems. The key person shall have skills and experience in the following mandatory areas Domain Skills Knowledge of the analytical principles for orbit determination and control of LEO spacecraft. Experience minimum 5 years in the definition of software requirements, architectural design, implementation and maintenance of Satellite Flight Dynamics Systems in the context of LEO missions based on the ESAIESOC NAPEOS Navigation Package for Earth Observation Satellite. Software Development, Verification Maintenance Skills Experience minimum 5 years in the full cycle of development and maintenance of application software, preferably for Satellite Flight Dynamics Systems, following formal software engineering processes. This includes user and system requirement analysis, software requirement engineering, software design, implementation, corrective and evolutive maintenance activities. Experience minimum 3 years in IV V integration, verification and validation activities for Flight Dynamics Systems following formal engineering processes. This includes requirement verification, system and subsystem integration, generation of test plan and test procedures, nonregression testing, generation of test data, generation of test tools, running the test procedures on the target system, generation of test reports and anomaly tracking. Software Engineering Skills Experience minimum 3 years in designing and developing software components and applications using Object Oriented 00 approach including design patterns. Experience minimum 3 years in designing and developing software applications using Java and related technologies. It would be a distinct advantage for the key person to have knowledge andor experience with some of the following Domain Skills Experience with software development and maintenance of Tools using the Orekit space dynamics library. Experience in integration of Flight Dynamics Systems with Mission Control Systems based on MICONYS software suite from ESAIESOC. Experience in integration of Flight Dynamics Systems with Mission Planning Systems. Experience with support to operations for Satellite Flight Dynamics Systems. System Maintenance Skills Experience in being the technical point of contact for contractors working at offsite premises and responsible for application software evolution and maintenance. Software Technology Skills IBM DOORS requirement management Tool. Experience in the usage of software CASE design tools e.g. Enterprise Architect andor MagicDraw. Experience in developing software applications using interfaces to relational database management systems RDBMS and experience with data model design for RDBMS. Unified Modelling Language UML for software design. Linux Operating System. XML processing schema design, validation, parser libraries, transformation XSLT and XPath. Experience in designing, developing and maintaining software client applications using Eclipse as HMI framework Rich Client Platform. Experience in designing and developing component based software applications using formal techniques e.g. OSGi. Experience using tools for the automation of software testing. The official languages are English and French. The working language for the position is English and therefore the key person must be able to work effectively in this language and have knowledge of the other. Good communication skills would be also an advantage. The key person shall also be assessed for the following skills and qualities Working proactively with the minimum of supervision in an individual or team environment. Conducting activities in an orderly and disciplined manner, working calmly and correctly under stress. Working in teams and sharing expertise and experience with other team members. Able to commit to the plan and deliver the expected results on time or to report proactively if any deviations are foreseen. Take ownership of problems through to effective resolution. Possess excellent verbal and written communications skills and be confident to deal with a wide variety of people. REFERENCE CFO016212176 LOCATION Darmstadt, Germany CONTACT recruitmoltek.net CLOSING DATE 8th April 2016 MOLTEK has been serving the space and aerospace industries since 1995, providing international consultancy services for a wide variety of clients from private and public corporations to national and international authorities and agencies.

Tags: system software flight engineer

 

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