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CONTROL with LIMITED INFORMATION ; SWITCHING ADAPTIVE CONTROL Daniel Liberzon Coordinated Science Laboratory and Dept. of Electrical & Computer Eng., Univ. of Illinois at Urbana-Champaign IAAC Workshop, Herzliya, Israel, June 1, 2009
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SWITCHING CONTROL Classical continuous feedback paradigm: u y P C u y P Plant: But logical decisions are often necessary: u y C1C1 C2C2 l o g i c P
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REASONS for SWITCHING Nature of the control problem Sensor or actuator limitations Large modeling uncertainty Combinations of the above
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REASONS for SWITCHING Nature of the control problem Sensor or actuator limitations Large modeling uncertainty Combinations of the above
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Plant Controller INFORMATION FLOW in CONTROL SYSTEMS
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Limited communication capacity many control loops share network cable or wireless medium microsystems with many sensors/actuators on one chip Need to minimize information transmission (security) Event-driven actuators Coarse sensing
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[ Brockett, Delchamps, Elia, Mitter, Nair, Savkin, Tatikonda, Wong,… ] Deterministic & stochastic models Tools from information theory Mostly for linear plant dynamics BACKGROUND Previous work: Unified framework for quantization time delays disturbances Our goals: Handle nonlinear dynamics
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Caveat: This doesn’t work in general, need robustness from controller OUR APPROACH (Goal: treat nonlinear systems; handle quantization, delays, etc.) Model these effects via deterministic error signals, Design a control law ignoring these errors, “Certainty equivalence”: apply control, combined with estimation to reduce to zero Technical tools: Input-to-state stability (ISS) Lyapunov functions Small-gain theorems Hybrid systems
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QUANTIZATION EncoderDecoder QUANTIZER finite subset of is partitioned into quantization regions
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QUANTIZATION and ISS
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– assume glob. asymp. stable (GAS) QUANTIZATION and ISS
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no longer GAS
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QUANTIZATION and ISS quantization error Assume class
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Solutions that start in enter and remain there This is input-to-state stability (ISS) w.r.t. measurement errors In time domain: QUANTIZATION and ISS quantization error Assume
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LINEAR SYSTEMS Quantized control law: 9 feedback gain & Lyapunov function Closed-loop: (automatically ISS w.r.t. )
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DYNAMIC QUANTIZATION
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– zooming variable Hybrid quantized control: is discrete state
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DYNAMIC QUANTIZATION – zooming variable Hybrid quantized control: is discrete state
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Zoom out to overcome saturation DYNAMIC QUANTIZATION – zooming variable Hybrid quantized control: is discrete state
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After ultimate bound is achieved, recompute partition for smaller region DYNAMIC QUANTIZATION – zooming variable Hybrid quantized control: is discrete state ISS from to small-gain condition Proof: Can recover global asymptotic stability
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QUANTIZATION and DELAY Architecture-independent approach Based on the work of Teel Delays possibly large QUANTIZER DELAY
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QUANTIZATION and DELAY where hence Can write
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SMALL – GAIN ARGUMENT if then we recover ISS w.r.t. [ Teel ’98 ] Small gain: Assuming ISS w.r.t. actuator errors: In time domain:
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FINAL RESULT Need: small gain true
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FINAL RESULT Need: small gain true
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FINAL RESULT solutions starting in enter and remain there Can use “zooming” to improve convergence Need: small gain true
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EXTERNAL DISTURBANCES [ Nešić–L ] State quantization and completely unknown disturbance
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EXTERNAL DISTURBANCES [ Nešić–L ] State quantization and completely unknown disturbance
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Issue: disturbance forces the state outside quantizer range Must switch repeatedly between zooming-in and zooming-out Result: for linear plant, can achieve ISS w.r.t. disturbance (ISS gains are nonlinear although plant is linear; cf. [ Martins ]) EXTERNAL DISTURBANCES [ Nešić–L ] State quantization and completely unknown disturbance After zoom-in:
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HYBRID SYSTEMS as FEEDBACK CONNECTIONS continuous discrete [ Nešić–L, ’05, ’06 ] Other decompositions possible Can also have external signals
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SMALL – GAIN THEOREM Small-gain theorem [ Jiang-Teel-Praly ’94 ] gives GAS if: Input-to-state stability (ISS) from to : ISS from to : (small-gain condition)
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SUFFICIENT CONDITIONS for IS S [ Hespanha-L-Teel ’08 ] # of discrete events on is ISS from to if: and ISS from to if ISS-Lyapunov function [ Sontag ’89 ] :
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LYAPUNOV – BASED SMALL – GAIN THEOREM Hybrid system is GAS if: and # of discrete events on is
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SKETCH of PROOF is nonstrictly decreasing along trajectories Trajectories along which is constant?None! GAS follows by LaSalle principle for hybrid systems [ Lygeros et al. ’03, Sanfelice-Goebel-Teel ’07 ]
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quantization error Zoom in: where ISS from to with gain small-gain condition! ISS from to with some linear gain APPLICATION to DYNAMIC QUANTIZATION
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RESEARCH DIRECTIONS Modeling uncertainty (with L. Vu) Disturbances and coarse quantizers (with Y. Sharon) Avoiding state estimation (with S. LaValle and J. Yu) Quantized output feedback Performance-based design Vision-based control (with Y. Ma and Y. Sharon) http://decision.csl.uiuc.edu/~liberzon
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REASONS for SWITCHING Nature of the control problem Sensor or actuator limitations Large modeling uncertainty Combinations of the above
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MODELING UNCERTAINTY Adaptive control (continuous tuning) vs. supervisory control (switching) unmodeled dynamics parametric uncertainty Also, noise and disturbance
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EXAMPLE Could also take controller index set Scalar system:, otherwise unknown (purely parametric uncertainty) Controller family: stable not implementable
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SUPERVISORY CONTROL ARCHITECTURE Plant Supervisor Controller u1u1 u2u2 umum y u...... candidate controllers...... – switching controller – switching signal, takes values in
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TYPES of SUPERVISION Prescheduled (prerouted) Performance-based (direct) Estimator-based (indirect)
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TYPES of SUPERVISION Prescheduled (prerouted) Performance-based (direct) Estimator-based (indirect)
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OUTLINE Basic components of supervisor Design objectives and general analysis Achieving the design objectives (highlights)
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OUTLINE Basic components of supervisor Design objectives and general analysis Achieving the design objectives (highlights)
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SUPERVISOR Multi- Estimator y1y1 y2y2 u y............ ypyp estimation errors: epep e2e2 e1e1...... Want to be small Then small indicates likely
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EXAMPLE Multi-estimator: exp fast =>
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EXAMPLE Multi-estimator: disturbance exp fast =>
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STATE SHARING Bad! Not implementable if is infinite The system produces the same signals
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SUPERVISOR...... Multi- Estimator y1y1 y2y2 ypyp epep e2e2 e1e1 u y............ Monitoring Signals Generator...... Examples:
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EXAMPLE Multi-estimator: – can use state sharing
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SUPERVISOR Switching Logic...... Multi- Estimator y1y1 y2y2 ypyp epep e2e2 e1e1 u y............ Monitoring Signals Generator...... Basic idea: Justification? small => small => plant likely in => gives stable closed-loop system (“certainty equivalence”) Plant, controllers:
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SUPERVISOR Switching Logic...... Multi- Estimator y1y1 y2y2 ypyp epep e2e2 e1e1 u y............ Monitoring Signals Generator...... Basic idea: Justification? small => small => plant likely in => gives stable closed-loop system only know converse! Need:small => gives stable closed-loop system This is detectability w.r.t. Plant, controllers:
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DETECTABILITY Want this system to be detectable “output injection” matrix asympt. stable view as output is Hurwitz Linear case: plant in closed loop with
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SUPERVISOR Switching Logic...... Multi- Estimator y1y1 y2y2 ypyp epep e2e2 e1e1 u y............ Monitoring Signals Generator...... Switching logic (roughly): This (hopefully) guarantees that is small Need:small => stable closed-loop switched system We know: is small This is switched detectability
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DETECTABILITY under SWITCHING need this to be asympt. stable plant in closed loop with view as output Assumed detectable for each frozen value of Output injection: slow switching (on the average) switching stops in finite time Thus needs to be “non-destabilizing” : Switched system: Want this system to be detectable:
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SUMMARY of BASIC PROPERTIES Multi-estimator: 1. At least one estimation error ( ) is small Candidate controllers: 3. is bounded in terms of the smallest : for 3, want to switch to for 4, want to switch slowly or stop conflicting when is bounded for bounded & Switching logic: 2. For each, closed-loop system is detectable w.r.t. 4. Switched closed-loop system is detectable w.r.t. provided this is true for every frozen value of
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SUMMARY of BASIC PROPERTIES Analysis: 1 + 3 => is small 2 + 4 => detectability w.r.t. => state is small Switching logic: Multi-estimator: Candidate controllers: 3. is bounded in terms of the smallest 4. Switched closed-loop system is detectable w.r.t. provided this is true for every frozen value of 2. For each, closed-loop system is detectable w.r.t. 1. At least one estimation error ( ) is small when is bounded for bounded &
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OUTLINE Basic components of supervisor Design objectives and general analysis Achieving the design objectives (highlights)
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Controller Plant Multi- estimator fixed CANDIDATE CONTROLLERS
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Linear: overall system is detectable w.r.t. if i.system inside the box is stable ii.plant is detectable fixed Plant Multi- estimator Controller P C E Need to show: => P C E,, => E C, i P ii =>
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CANDIDATE CONTROLLERS Linear: overall system is detectable w.r.t. if i.system inside the box is stable ii.plant is detectable fixed Plant Multi- estimator Controller P C E Nonlinear: same result holds if stability and detectability are interpreted in the ISS / OSS sense: external signal
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CANDIDATE CONTROLLERS Linear: overall system is detectable w.r.t. if i.system inside the box is stable ii.plant is detectable fixed Plant Multi- estimator Controller P C E Nonlinear: same result holds if stability and detectability are interpreted in the integral-ISS / OSS sense:
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SWITCHING LOGIC: DWELL-TIME Obtaining a bound on in terms of is harder Not suitable for nonlinear systems (finite escape) Initialize Find no ? yes – monitoring signals – dwell time Wait time units Detectability is preserved if is large enough
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SWITCHING LOGIC: HYSTERESIS Initialize Find no yes – monitoring signals – hysteresis constant ? or (scale-independent)
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SWITCHING LOGIC: HYSTERESIS This applies to exp fast, finite, bounded switching stops in finite time => Initialize Find no yes ? Linear, bounded average dwell time =>
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