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  • IAC-20
  • D1
  • 4A
  • session 4A

    Title

    Space Systems Engineering - Methods, Processes and Tools (1)

    Description

    This session will focus on state-of-the-art systems engineering methodologies that reduce the time and cost, and improve the quality of space system design. Of special interest are multi-disciplinary methods, processes, and tools used for System Design, Product Realization, Technical Management, Operations, and Retirement of space systems to improve risk management, safety, reliability, testability, and quality of life cycle cost estimates. Specifically, presentations may include: state of organizational structures, practice methods, processes, tools, training that benefit space system design, development and operations; state of the art systems engineering methodologies for space systems, including space system(s) of systems (SoS); engineering design methods or modeling and simulation tools applied to space system design and optimization; methodologies and processes for technical planning, control, assessment and decision analysis of space system design; advancement in space system development environments, such as concurrent engineering design facilities; and novel methods to improve risk management, earned value management, configuration management, data management, availability, safety, reliability, testability and quality of life cycle cost estimates.

    IPC members
    • Co-Chair: Dr. Dapeng Wang, Beihang University, China;

    • Co-Chair: Mr. Peter Dieleman, Netherlands Aerospace Centre (NLR), The Netherlands;

    • Rapporteur: Mr. Franck Durand-Carrier, Centre National d'Etudes Spatiales (CNES), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A modular system design and analysis approach for sizing commercial post-ISS LEO infrastructures

    16

    withdrawn

    Mr. Andy Braukhane

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    2

    systems engineering applied to orbit and attitude control system (aocs) of formation flying satellites

    16

    confirmed

    Mr. Iván Felipe Rodríguez Barón

    National Institute for Space Research - INPE

    Brazil

    3

    Multi-attribute Evaluation Approach for Small Launch Vehicle with Multi-objective Multi-discipline Design Optimization

    16

    confirmed

    Dr. Hao Zhu

    Beihang University (BUAA)

    China

    4

    Uncertainty design and optimization of small hybrid launch vehicles based on polynomial chaos expansion

    16

    withdrawn

    Mr. Mingyang Xiao

    Beihang University (BUAA)

    China

    5

    Technology assessment and prioritization for space architectures

    16

    withdrawn

    Dr. Cesare Guariniello

    Purdue University

    United States

    6

    Digital Engineering Information Exchange Model for Space Missions Architecture: a Case Study of a CubeSat Mission

    16

    confirmed

    Mr. Yaroslav Menshenin

    Skolkovo Institute of Science and Technology

    Russian Federation

    7

    accelerate spacecraft prox-ops design and analysis with soda

    16

    Dr. nazareth bedrossian

    United States

    8

    Mission-aware Digital Continuum in Systems Design with Data-driven Systems Engineering and Digital Mission Engineering

    16

    confirmed

    Mr. Kuldeep Rambhai Barad

    Delft University of Technology (TU Delft)

    The Netherlands

    9

    CUBESAT THERMAL MANAGEMENT SYSTEM DESIGN SUPPORTED BY MULTIDISCIPLINARY DESIGN OPTIMISATION

    16

    confirmed

    Mr. Daniele Calvi

    Politecnico di Torino

    Italy

    10

    A novel approach to planetary rover guidance, navigation and control based on the estimation of the remaining useful life

    16

    confirmed

    Ms. Jasmine Rimani

    Politecnico di Torino

    Italy

    11

    multidisciplinary optimization for nano-satellite launch vehicles

    16

    confirmed

    Mr. Daniel McCammon

    C6 Launch Systems

    Canada

    12

    Vision of a Next-Gen Concurrent Design Facility

    withdrawn

    Dr. Loveneesh Rana

    University of Luxembourg

    Luxembourg

    13

    Automatic RF Ion Thruster Accelerated Development Chain

    confirmed

    Mr. Ruslan Rakhimov

    Skolkovo Institute of Science and Technology

    Russian Federation