Control reconfiguration

Control reconfiguration is an active approach in control theory to achieve fault-tolerant control for dynamic systems. ^[1] It is used when severe faults, such as actuator or sensor outages, cause a break-up of the control loop, which must be restructured to prevent failure at the system level. In addition to loop restructuring, the controller parameters must be adjusted to accommodate changed plant dynamics. Control reconfiguration is a building block toward increasing the dependability of systems under feedback control. ^[2]

Reconfiguration problem

Schematic diagram of a typical active fault-tolerant control system. In the nominal, i.e. fault-free situation, the lower control loop operates to meet the control goals. The fault-detection (FDI) module monitors the closed-loop system to detect and isolate faults. The fault estimate is passed to the reconfiguration block, which modifies the control loop to reach the control goals in spite of the fault.

Fault modelling

The figure to the right shows a plant controlled by a controller in a standard control loop.

The nominal linear model of the plant is

${\displaystyle {\begin{cases}{\dot {\mathbf {x} }}&=\mathbf {A} \mathbf {x} +\mathbf {B} \mathbf {u} \\\mathbf {y} &=\mathbf {C} \mathbf {x} \end{cases}}}$

The plant subject to a fault (indicated by a red arrow in the figure) is modelled in general by

${\displaystyle {\begin{cases}{\dot {\mathbf {x} }}_{f}&=\mathbf {A} _{f}\mathbf {x} _{f}+\mathbf {B} _{f}\mathbf {u} \\\mathbf {y} _{f}&=\mathbf {C} _{f}\mathbf {x} _{f}\end{cases}}}$

where the subscript ${\displaystyle f}$ indicates that the system is faulty. This approach models multiplicative faults by modified system matrices. Specifically, actuator faults are represented by the new input matrix ${\displaystyle \mathbf {B} _{f}}$, sensor faults are represented by the output map ${\displaystyle \mathbf {C} _{f}}$, and internal plant faults are represented by the system matrix ${\displaystyle \mathbf {A} _{f}}$.

The upper part of the figure shows a supervisory loop consisting of fault detection and isolation (FDI) and reconfiguration which changes the loop by

1. choosing new input and output signals from {${\displaystyle \mathbf {u} ,\mathbf {y} }$} to reach the control goal,
2. changing the controller internals (including dynamic structure and parameters),
3. adjusting the reference input ${\displaystyle \mathbf {w} }$.

To this end, the vectors of inputs and outputs contain all available signals, not just those used by the controller in fault-free operation.

Alternative scenarios can model faults as an additive external signal ${\displaystyle \mathbf {f} }$ influencing the state derivatives and outputs as follows:

${\displaystyle {\begin{cases}{\dot {\mathbf {x} }}_{f}&=\mathbf {A} \mathbf {x} _{f}+\mathbf {B} \mathbf {u} +\mathbf {E} \mathbf {f} \\\mathbf {y} _{f}&=\mathbf {C} _{f}\mathbf {x} _{f}+\mathbf {F} \mathbf {f} \end{cases}}}$

Reconfiguration goals

The goal of reconfiguration is to keep the reconfigured control-loop performance sufficient for preventing plant shutdown. The following goals are distinguished:

1. Stabilization
2. Equilibrium recovery
3. Output trajectory recovery
4. State trajectory recovery
5. Transient time response recovery

Internal stability of the reconfigured closed loop is usually the minimum requirement. The equilibrium recovery goal (also referred to as weak goal) refers to the steady-state output equilibrium which the reconfigured loop reaches after a given constant input. This equilibrium must equal the nominal equilibrium under the same input (as time tends to infinity). This goal ensures steady-state reference tracking after reconfiguration. The output trajectory recovery goal (also referred to as strong goal) is even stricter. It requires that the dynamic response to an input must equal the nominal response at all times. Further restrictions are imposed by the state trajectory recovery goal, which requires that the state trajectory be restored to the nominal case by the reconfiguration under any input.

Usually a combination of goals is pursued in practice, such as the equilibrium-recovery goal with stability.

The question whether or not these or similar goals can be reached for specific faults is addressed by reconfigurability analysis.

Reconfiguration approaches

Fault hiding

Fault hiding principle. A reconfiguration block is placed between faulty plant and nominal controller. The reconfigured plant behaviour must match the nominal behaviour. Furthermore, the reconfiguration goals are pointed out.

This paradigm aims at keeping the nominal controller in the loop. To this end, a reconfiguration block can be placed between the faulty plant and the nominal controller. Together with the faulty plant, it forms the reconfigured plant. The reconfiguration block has to fulfill the requirement that the behaviour of the reconfigured plant matches the behaviour of the nominal, that is fault-free plant. ^[3]

Linear model following

In linear model following, a formal feature of the nominal closed loop is attempted to be recovered. In the classical pseudo-inverse method, the closed loop system matrix ${\displaystyle {\bar {\mathbf {A} }}=\mathbf {A} -\mathbf {B} \mathbf {K} }$ of a state-feedback control structure is used. The new controller ${\displaystyle \mathbf {K} _{f}}$ is found to approximate ${\displaystyle {\bar {\mathbf {A} }}}$ in the sense of an induced matrix norm. ^[4]

In perfect model following, a dynamic compensator is introduced to allow for the exact recovery of the complete loop behaviour under certain conditions.

In eigenstructure assignment, the nominal closed loop eigenvalues and eigenvectors (the eigenstructure) is recovered to the nominal case after a fault.

Optimisation-based control schemes

Optimisation control schemes include: linear-quadratic regulator design (LQR), model predictive control (MPC) and eigenstructure assignment methods. ^[5]

Probabilistic approaches

Some probabilistic approaches have been developed. ^[6]

Learning control

There are learning automata, neural networks, etc. ^[7]

Mathematical tools and frameworks

The methods by which reconfiguration is achieved differ considerably. The following list gives an overview of mathematical approaches that are commonly used. ^[8]

• Adaptive control (AC)
• Disturbance decoupling (DD)
• Eigenstructure assignment (EA)
• Gain scheduling (GS)/linear parameter varying (LPV)
• Generalised internal model control (GIMC)
• Intelligent control (IC)
• Linear matrix inequality (LMI)
• Linear-quadratic regulator (LQR)
• Model following (MF)
• Model predictive control (MPC)
• Pseudo-inverse method (PIM)
• Robust control techniques

See also

Prior to control reconfiguration, it must be at least determined whether a fault has occurred (fault detection) and if so, which components are affected (fault isolation). Preferably, a model of the faulty plant should be provided (fault identification). These questions are addressed by fault diagnosis methods.

Fault accommodation is another common approach to achieve fault tolerance. In contrast to control reconfiguration, accommodation is limited to internal controller changes. The sets of signals manipulated and measured by the controller are fixed, which means that the loop cannot be restructured. ^[9]

References

1. ( Blanke et al. 2006 )
2. ( Patton 1997 )
3. ( Steffen 2005 )
4. ( Gao & Antsaklis 1991 )( Staroswiecki 2005 )
5. ( Looze et al. 1985 )( Lunze, Rowe-Serrano & Steffen 2003 )( Esna Ashari, Khaki Sedigh & Yazdanpanah 2005 )( Maciejowski & Jones 2003 )
6. ( Mahmoud, Jiang & Zhang 2003 )
7. ( Rauch 1994 )
8. ( Zhang & Jiang 2003 )
9. ( Blanke et al. 2006 )

Further reading

• Blanke, M.; Kinnaert, M.; Lunze, J.; Staroswiecki, M. (2006), Diagnosis and Fault-Tolerant Control (2nd ed.), Springer
• Steffen, T. (2005), Control Reconfiguration of Dynamical Systems, Springer
• Staroswiecki, M. (2005), "Fault Tolerant Control: The Pseudo-Inverse Method Revisited", Proceedings of the 16th IFAC World Congress, Prague, Czech Republic: IFAC
• Lunze, J.; Rowe-Serrano, D.; Steffen, T. (2003), "Control Reconfiguration Demonstrated at a Two-Degrees-of-Freedom Helicopter Model", Proceedings of European Control Conference (ECC), Cambridge, UK.
• Maciejowski, J.; Jones, C. (2003), "MPC Fault-Tolerant Flight Control Case Study: Flight 1862", Proceedings of the SAFEPROCESS 2003: 5th Symposium on Detection and Safety for Technical Processes, Washington D.C., USA: IFAC, pp. 265–276
• Mahmoud, M.; Jiang, J.; Zhang, Y. (2003), Active Fault Tolerant Control Systems - Stochastic Analysis and Synthesis, Springer
• Zhang, Y.; Jiang, J. (2003), "Bibliographical review on reconfigurable fault-tolerant control systems", Proceedings of the SAFEPROCESS 2003: 5th Symposium on Detection and Safety for Technical Processes, Washington D.C., USA: IFAC, pp. 265–276
• Patton, R. J. (1997), "Fault-tolerant control: the 1997 situation", Preprints of IFAC Symposium on Fault Detection Supervision and Safety for Technical Processes, Kingston upon Hull, UK, pp. 1033–1055
• Rauch, H. E. (1995), "Autonomous control reconfiguration", IEEE Control Systems Magazine, 15 (6): 37–48, doi:10.1109/37.476385
• Rauch, H. E. (1994), "Intelligent fault diagnosis and control reconfiguration", IEEE Control Systems Magazine, 14 (3): 6–12, doi:10.1109/37.291462, S2CID   39931526
• Gao, Z.; Antsaklis, P.J. (1991), "Stability of the pseudo-inverse method for reconfigurable control systems", International Journal of Control, 53 (3): 717–729, doi:10.1080/00207179108953643
• Looze, D.; Weiss, J.L.; Eterno, J.S.; Barrett, N.M. (1985), "An Automatic Redesign Approach for Restructurable Control Systems", IEEE Control Systems Magazine, 5 (2): 16–22, doi:10.1109/mcs.1985.1104940, S2CID   12684489 .
• Esna Ashari, A.; Khaki Sedigh, A.; Yazdanpanah, M. J. (2005), "Reconfigurable control system design using eigenstructure assignment: static, dynamic and robust approaches", International Journal of Control, 78 (13): 1005–1016, doi:10.1080/00207170500241817, S2CID   121350006 .