Spacecraft health monitoring and management systems

Spacecraft health monitoring and management systems (also referred to as FDIR (Fault Detection, Isolation and Recovery) systems)) are addressed since the very beginning of any space mission design and play a relevant role in the definition of their reliability, availability and safety objectives. Their primary purposes are the safety of spacecraft/mission life and the improvement of its service availability. In this paper current technical and programmatic FDIR strategies are presented along with their strong connection with the wider concept of on-board autonomy, which is becoming the key-point in the design of new-generation spacecrafts. Recent projects developed at OHB System AG have brought to light some issues in the current FDIR system design approaches. These findings pave the way for innovative solutions, which can support and not rule out conventional industrial practices.

[1]  Joseph Sifakis,et al.  Formal methods for the validation of fault tolerance in autonomous spacecraft , 1996, Proceedings of Annual Symposium on Fault Tolerant Computing.

[2]  E. Denney,et al.  Verification of autonomous systems for space applications , 2006, 2006 IEEE Aerospace Conference.

[3]  Julien Marzat,et al.  Model-based fault diagnosis for aerospace systems: a survey , 2012 .

[4]  Joseph Sifakis,et al.  Compositional Verification for Component-Based Systems and Application , 2008, ATVA.

[5]  Xavier Olive,et al.  FDI(R) for satellites: How to deal with high availability and robustness in the space domain? , 2012, Int. J. Appl. Math. Comput. Sci..

[6]  Fatemeh SalarKaleji,et al.  A survey on Fault Detection, Isolation and Recovery (FDIR) module in satellite onboard software , 2013, 2013 6th International Conference on Recent Advances in Space Technologies (RAST).

[7]  Xavier Olive FDIR for satellites , 2012 .

[8]  Inseok Hwang,et al.  A Survey of Fault Detection, Isolation, and Reconfiguration Methods , 2010, IEEE Transactions on Control Systems Technology.