Grzegorz Chlewicki

External Consultant - Satellite Software and Engineering

Grzegorz Chlewicki is an external consultant with long-standing experience in spacecraft system engineering, with particular expertise in AOCS, avionics, and on-board autonomy. He holds a Ph.D. in Astrophysics from the University of Leiden and has been active in the European space industry for more than three decades, contributing to major scientific and commercial missions. His experience covers all phases of spacecraft development, including system and subsystem design, specification and implementation of on-board software and FDIR functions, AIT/AIV, launch campaigns, and in-orbit operations support. He has held senior engineering and system roles on major missions such as Euclid, Galileo, Herschel–Planck, BeppoSAX, and ASTRA 1K. His technical contributions include the definition of onboard autonomy, FDIR, and contingency-handling concepts for science missions with stringent reliability requirements, as well as the resolution of critical AOCS and avionics design issues. He was the design leader of the gyroless AOCS for Beppo SAX (safe and science observations mode), which allowed the spacecraft to continue operations after multiple gyroscope failures and to exceed nearly three times the planned duration of the mission.

P&P Software GmbH
Rheinsichtweg 8
Taegerwilen, 8274 (CH)

Phone: +41 78 626 27 05
Fax: +41 71 669 16 93
Email: pasetti@pnp-software.com

Education

PhD in Astrophysics / University of Leiden
1985
Master's degree in Astronomy / N. Copernicus University, Toruń
1979

Career History

Independent consultant / contractor for space industry projects
From 1991
Software consultant HCS Industrial Automation
1989-1991
Software systems analyst BSO Aerospace and Systems
1989

Selected projects and technical contributions

Avionics/AOCS/spacecraft system engineer Euclid
2012-22
  • Design of system autonomy and FDIR approach
  • Design of critical levels of system FDIR; development of spacecraft safety strategy relying on the use of software for major system contingencies and moving away from the hardware-based approach used on previous ESA science missions
  • Contributions to spacecraft system specifications and the definition and procurement of avionics hardware (onboard computer)
  • Analysis of attitude contingencies in the post-separation phase, analysis of launch windows to cope with specific launcher and spacecraft constraints
  • Contributions to the specification of spacecraft onboard software, including FDIR, and logic and algorithms for individual subsystems (thermal control)
  • Engineering support for AOCS closed loop tests executed on EM and FM spacecraft including development of software for detailed analysis of AOCS and system test data
Functional system AIV engineer Galileo IOV
2009-12
  • Providing engineering support for all functional system tests of Galileo IOV spacecraft
  • Contributions to the definition and implementation of the spacecraft launch configuration sequence
  • Providing support at launch site as avionics / system engineer for both IOV launch campaigns
AOCS system engineer Herschel-Planck
2001-2009
  • Definition of AOCS requirements and interfaces with spacecraft service modules (onboard computer, RCS)
  • Follow-up of AOCS development including AOCS software and system-level validation
  • System level analyses related to the AOCS and system performance (pointing budget, empirical thrust modelling, active control of thruster temperatures for Planck)
  • Definition of operational aspects of the AOCS
  • Engineering support in ESOC during LEOP and in-orbit commissioning
AOCS manager / System dynamics architect ASTRA 1K
1998-2001
  • Definition of subsystem requirements due to enhancements of standard Spacebus architecture (RF sensing, electrical propulsion)
  • Management of AOCS development, including software and coordination of hardware procurement
  • Engineering support for system-level AOCS tests in AIV
  • System level analyses related to the AOCS (thruster positioning and selection for manoeuvres, effects of close collocation of spacecraft on the AOCS)
AOCS engineer Beppo SAX
1991-1998
  • Development, execution and engineering analysis of closed loop tests on the AOCS subsystem test bench
  • Specification and support for the implementation spacecraft dynamic simulator used in AOCS tests
  • AOCS engineering support during in-orbit commissioning
  • Principal designer and developer of gyroless AOCS modes allowing continuation of spacecraft mission following multiple gyroscope failures
  • Design and implementation of critical algorithms for the gyroless AOCS: star pattern recognition and attitude determination, open loop disturbance torque compensation

Scientific Research

Research interests

  • • Modelling of interstellar dust particles
  • • Radiation transfer
  • • Modelling of infrared emission from the interstellar medium
  • • Interstellar optical polarisation
  • • Satellite UV spectrocopy of stars
  • • Ground-based spectroscopy of interstellar features
  • • Satellite IR photometry of the interstellar medium

Publications

  • • Science: 35 published contributions including articles in astrophysical journals, review papers and conference presentations
  • • Engineering: Conference presentations related to participation in major missions