advanced spacecraft systems design using model-based

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Advanced Spacecraft Systems Design using Model-based Techniques Volker Schaus, Daniel Lüdtke, Andreas Gerndt German Aerospace Center (DLR) Simulation and Software Technology Software for Space Systems and Interactive Visualization Federated Satellite Systems Workshop 14 th Oct 2014 > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de Chart 1

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PowerPoint-Präsentation 16:9 EnglischSimulation and Software Technology Software for Space Systems and Interactive Visualization Federated Satellite Systems Workshop 14th Oct 2014
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 1
Systems Engineering
Image: DLR.de
Used for preliminary aircraft design studies, air traffic management and scenario analyses
Flexible arrangement of desks depending on study requirements
Currently: Focus on multi- disciplinary design and optimization
Source: e.g. TSTI
Taking Advantage of the Model-based Approach
Documents vs Models
Adding Semantics – Unit Management Example
*Volker Schaus, Philipp M. Fischer, Andreas Gerndt - Taking Advantage of the Model: Application of the Quantity, Units, Dimension, and Values Standard in Concurrent Spacecraft Engineering – INCOSE International Symposium 2013, Philadelphia, PA
Integration of the Quantity, Units, Dimension, and Values Standard (QUDV)
Automatic Unit Conversion
Sanity Checks
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 7
Usage in the Software Virtual Satellite > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 8
System(s) Analyis
Sensitivity Analysis
*Volker Schaus, Philipp M. Fischer, Dominik Quantius, Andreas Gerndt - Automated Sensitivity Analysis in Early Space Mission Design – SECESA Workshop 2012, Lisbon, Portugal
Dependency analysis
Enables informed decision making
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 10
Decision Support
*Meenakshi Deshmukh, Volker Schaus, Philipp M. Fischer, Dominik Quantius, Volker Maiwald, Andreas Gerndt - Decision Support Tool for Concurrent Engineering in Space Mission Design - 19th ISPE International Conference on Concurrent Engineering, Trier, Germany
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 11
Software Engineering
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 12
State Machine
Informed Search
Algorithm Result
Image: DLR.de
State Explosion *Philipp M. Fischer, Daniel Lüdtke, Volker Schaus, Andreas Gerndt - A Formal
Method for Early Spacecraft Design Verification – IEEE Aerospace 2013
Formal Verification in the Space Domain > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 13
Adding Verification to the CE core team > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 14
What is Virtual Satellite? – CE Software Tool
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 15
Work Process
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 16
*Volker Schaus, Michael Tiede, Philipp M. Fischer, Andreas Gerndt - A Continuous Verification Process in Concurrent Engineering – AIAA Space 2013, Sane Diego
Defining the Verification Model – Running the Search
Charge Power = 80 [W]
Duration = 20 [min]
Duration = 60 [min]
Describe Operational Goals
Parameter TotalDownlinkData Above 10000.0; Parameter MissionTime Below 365.0; End Describe Operational Constraints Constraint BatteryChargeConstraint for Parameter batteryCharge Between 40.0 And 240.0 ; End
Req.: 10 GB of data in one year Con.: Max. battery capacity 240 Ah Con.: Min. charge level 40Ah
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 17
Ti m
e Co
ns tr
ai nt
Battery Constraint
Battery Constraint
Experiment
Ti m
e Co
ns tr
ai nt
Experiment
Generation of Project Related Artifacts
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 20
Collaborative Configuration supported by Interactive Visualization
Integrated visualization model
Publication at IEEExplore
Saves time for configuration engineer
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 22
Motivation: Data Model and the References
> Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 23
Current State
Interface Diagram > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 25
Discipline providing the
Internal Block Diagram > Advanced Spacecraft Systems Design using Model-based Techniques > Volker Schaus > 14th Oct 2014 DLR.de • Chart 26
→ →
Integration in the Software
Summary
Model-based Systems Engineering, Concurrent Engineering • Space, Aircraft Design, …
Semantics • QUDV example • Early Verification
System Analysis • Sensitivity • Decision Support • Dependency Visualization with Diagrams
Artifact Generation • Geometric Model
Questions ? [email protected]
Systems Engineering
Usage in the Software Virtual Satellite
System(s) Analyis
Foliennummer 10
Decision Support
Software Engineering
Adding Verification to the CE core team
Foliennummer 15
Work Process
Result – Sequence of Mode Switches
Result – Sequence of Mode Switches
Generation of Project Related Artifacts
Collaborative Configuration supported by Interactive Visualization
CAD Interface: CATIA Export
Current State
Interface Diagram