A class of nonlinear unknown input observer for fault diagnosis: Application to fault tolerant control of an autonomous spacecraft

In this paper, the problem of Nonlinear Unknown Input Observer (NUIO) based Fault Detection and Isolation (FDI) scheme design for a class of nonlinear Lipschitz systems is studied. The proposed FDI method is applied to detect, isolate and accommodate thruster faults of an autonomous spacecraft involved in the rendezvous phase of the Mars Sample Return (MSR) mission. Considered fault scenarios represent fully closed thruster and thruster efficiency loss. The FDI scheme consists of a bank of NUIOs with adjustable error dynamics, a robust fault detector that is based on judiciously chosen frame and an isolation logic. The bank of observers is in charge of confining the fault to a subset of possible faults and the isolation logic makes the final decision about the faulty thruster index. Finally, a thruster fault is accommodated by re-allocating the desired forces and torques among the remaining healthy thrusters and closing the associated thruster valve. Monte Carlo results from “high-fidelity” MSR industrial simulator demonstrate that the proposed fault tolerant strategy is able to accommodate thruster faults that may have effect on the final rendezvous criteria.

[1]  M. Darouach,et al.  Full-order observers for linear systems with unknown inputs , 1994, IEEE Trans. Autom. Control..

[2]  Steven X. Ding,et al.  Model-based Fault Diagnosis Techniques: Design Schemes, Algorithms, and Tools , 2008 .

[3]  D. Henry Fault Diagnosis of Microscope Satellite Thrusters Using H∞ /H_ Filters , 2008 .

[4]  Eric Bornschlegl,et al.  Robust Fault Diagnosis strategies for Spacecraft Application to LISA Pathfinder experiment , 2010 .

[5]  Xavier Olive FDIR for satellites , 2012 .

[6]  Stéphane Ploix,et al.  Fault diagnosis and fault tolerant control , 2007 .

[7]  D. Henry Fault Diagnosis of Microscope Satellite Thrusters Using H-infinity/H_ Filters , 2008 .

[8]  Eric Bornschlegl,et al.  Thruster Fault Detection, Isolation and Accommodation for an Autonomous Spacecraft , 2014 .

[9]  Dusan Krokavec,et al.  On the Takagi-Sugeno model-based state estimation for one class of bilinear systems , 2013, Proceedings of the 14th International Carpathian Control Conference (ICCC).

[10]  Ping Lu,et al.  Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation , 2001 .

[11]  M. Hou,et al.  Design of observers for linear systems with unknown inputs , 1992 .

[12]  M. Saif,et al.  Unknown input observer design for a class of nonlinear systems: an LMI approach , 2006, American Control Conference.

[13]  Mehrdad Saif,et al.  Observer-Based Fault Diagnosis of Satellite Systems Subject to Time-Varying Thruster Faults , 2007 .

[14]  P. Gahinet,et al.  H∞ design with pole placement constraints: an LMI approach , 1996, IEEE Trans. Autom. Control..

[15]  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..

[16]  Youmin Zhang,et al.  Bibliographical review on reconfigurable fault-tolerant control systems , 2003, Annu. Rev. Control..

[17]  Eric Bornschlegl,et al.  Robust Fault Diagnosis for Systems with Electronic Induced Delays , 2012 .

[18]  H. Marquez,et al.  Design of unknown input observers for Lipschitz nonlinear systems , 2005, Proceedings of the 2005, American Control Conference, 2005..

[19]  Eric Bornschlegl,et al.  Robust fault detection for systems with electronic induced delays: Application to the rendezvous phase of the MSR mission , 2013, 2013 European Control Conference (ECC).