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Hybrid Systems Modeling, Analysis, Control. Datta Godbole, John Lygeros, Claire Tomlin, Gerardo Lafferiere, George Pappas, John Koo Jianghai Hu, Rene Vidal, Shawn Shaffert, Jun Zhang, Slobodan Simic, Kalle Johansson, Maria Prandini
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Hybrid Systems Modeling, Analysis, Control Datta Godbole, John Lygeros, Claire Tomlin, Gerardo Lafferiere, George Pappas, John Koo Jianghai Hu, Rene Vidal, Shawn Shaffert, Jun Zhang, Slobodan Simic, Kalle Johansson, Maria Prandini David Shim, Jin Kim, Omid Shakernia, Cedric Ma, Judy Liebmann and Ben Horowitz (with the interference of) Shankar Sastry
What Are Hybrid Systems? • Dynamical systems with interacting continuous and discrete dynamics
Why Hybrid Systems? • Modeling abstraction of • Continuous systems with phased operation (e.g. walking robots, mechanical systems with collisions, circuits with diodes) • Continuous systems controlled by discrete inputs (e.g. switches, valves, digital computers) • Coordinating processes (multi-agent systems) • Important in applications • Hardware verification/CAD, real time software • Manufacturing, chemical process control, • communication networks, multimedia • Large scale, multi-agent systems • Automated Highway Systems (AHS) • Air Traffic Management Systems (ATM) • Uninhabited Aerial Vehicles (UAV), Power Networks
Control Challenges • Large number of semiautonomous agents • Coordinate to • Make efficient use of common resource • Achieve a common goal • Individual agents have various modes of operation • Agents optimize locally, coordinate to resolve conflicts • System architecture is hierarchical and distributed • Safety critical systems Challenge: Develop models, analysis, and synthesis tools for designing and verifying the safety of multi-agent systems
Control Theory Computer Science Models of computation Control of individual agents Communication models Continuous models Discrete event systems Differential equations Hybrid Systems Proposed Framework
Automated Highway Systems • Goal • Increase highway throughput • Same highway infrastructure • Same level of safety • Same level of passenger comfort • Introduce automation • Partial: driver assistance, intelligent cruise control, warning system • Full: individual vehicles, mixed traffic, platooning • Complex problem • Technological issues (is it possible with current technology) • Social/Political issues (insurance and legal issues, equality)
Safety-Throughput Tradeoff • Contradictory demands • Safety: vehicles far and moving slowly • Throughput: vehicles close and moving fast • Proposed compromise • Allow low relative velocity collisions • In emergency situations • Two possible safe arrangements • Large spacing (leader mode) • Small spacing (follower mode) • Platooning concept
Control Hierarchy • Implementation requires automatic control • Control hierarchy proposed in [Varaiya 93] • Regulation layer: braking, acceleration and steering • Coordination layer: maneuvers implemented by communication protocols • Link layer: flow control, lane assignment • Network layer: routing • Hybrid phenomena appear throughout • Switching controllers for regulation • Switching between maneuvers • Lane and maneuver assignment • Degraded modes of operation
Air Traffic Management Systems • Studied by NEXTOR and NASA • Increased demand for air travel • Higher aircraft density/operator workload • Severe degradation in adverse conditions • High business volume • Technological advances: Guidance, Navigation & Control • GPS, advanced avionics, on-board electronics • Communication capabilities • Air Traffic Controller (ATC) computation capabilities • Greater demand and possibilities for automation • Operator assistance • Decentralization • Free flight
Current ATM System CENTER B CENTER A TRACON VOR SUA 20 Centers, 185 TRACONs, 400 Airport Towers Size of TRACON: 30-50 miles radius, 11,000ft Centers/TRACONs are subdivided to sectors Approximately 1200 fixed VOR nodes Separation Standards Inside TRACON : 3 miles, 1,000 ft Below 29,000 ft : 5 miles, 1,000ft Above 29,000 ft : 5 miles, 2,000ft TRACON GATES Computable Hybrid Systems
In the presence of the predicted soaring demand for air travel, the above problems will be greatly amplified leading to both safety and performance degradation in the future Current ATM System Limitations • Inefficient Airspace Utilization • Nondirect, wind independent, nonoptimal routes • Centralized System Architecture • Increased controller workload resulting in holding patterns • Obsolete Technology and Communications • Frequent computer and display failures • Limitations amplified in oceanic airspace • Separation standards in oceanic airspace are very conservative Computable Hybrid Systems
A Future ATM Concept CENTER B • FreeFlight from TRACON to TRACON • Increases airspace utilization • Tools for optimizing TRACON capacity • Increases terminal area capacity and throughput • Decentralized Conflict Prediction & Resolution • Reduces controller workload and increases safety CENTER A TRACON ALERT ZONE PROTECTED ZONE TRACON Computable Hybrid Systems
Hybrid Systems in ATM • Automation requires interaction between • Hardware (aircraft, communication devices, sensors, computers) • Software (communication protocols, autopilots) • Operators (pilots, air traffic controllers, airline dispatchers) • Interaction is hybrid • Mode switching at the autopilot level • Coordination for conflict resolution • Scheduling at the ATC level • Degraded operation • Requirement for formal design and analysis techniques • Safety critical system • Large scale system
Control Hierarchy • Flight Management System (FMS) • Regulation & trajectory tracking • Trajectory planning • Tactical planning • Strategic planning • Decentralized conflict detection and resolution • Coordination, through communication protocols • Air Traffic Control • Scheduling • Global conflict detection and resolution
Hybrid Research Issues • Hierarchy design • FMS level • Mode switching • Aerodynamic envelope protection • Strategic level • Design of conflict resolution maneuvers • Implementation by communication protocols • ATC level • Scheduling algorithms (e.g. for take-offs and landings) • Global conflict resolution algorithms • Software verification • Probabilistic analysis and degraded modes of operation
Other Applications • Uninhabited Aerial Vehicles (UAV) • Automated aerial vehicles (airplanes and/or helicopters) • Coordinate for search and rescue, or seek and destroy missions • Control hierarchy similar to ATM • Mode switching, discrete coordination, flight envelope protection • Power Electronic Building Blocks (PEBB) • Power electronics, with sensing, control, communication • Improve power network efficiency and reliability for utilities, hybrid electric vehicle, universal power ships • Control hierarchy: load balancing/shedding, network stabilization, pulse width modulation • Hybrid phenomena: modulation, input characteristic switching, scheduling
Wireless LAN TCP/IP TCP/IP WIRELESS HUB GROUNDSTATION VIRTUAL COCKPIT GRAPHICAL EMMULATION UAV Laboratory Configuration
Motivation • Goal • Design a multi-agent multi-modal control system for Unmanned Aerial Vehicles (UAVs) • Intelligent coordination among agents • Rapid adaptation to changing environments • Interaction of models of operation • Guarantee • Safety • Performance • Fault tolerance • Mission completion Conflict Resolution Collision Avoidance Envelope Protection Tracking Error Fuel Consumption Response Time Sensor Failure Actuator Failure Path Following Object Searching Pursuit-Evasion
Hierarchical Hybrid Systems • Envelope Protecting Mode • Normal Flight Mode Tactical Planner Safety Invariant Liveness Reachability
The UAV Aerobot Club at Berkeley • Architecture for multi-level rotorcraft UAVs 1996- to date • Pursuit-evasion games 2000- to date • Landing autonomously using vision on pitching decks 2001- to date • Multi-target tracking 2001- to date • Formation flying and formation change 2002
Hybrid Automata • Hybrid Automaton • State space • Input space • Initial states • Vector field • Invariant set • Transition relation • Remarks: • countable, • State • Can add outputs, etc. (not needed here)
Executions • Hybrid time trajectory, , finite or infinite with • Execution with and • Initial Condition: • Discrete Evolution: • Continuous Evolution: over , continuous, piecewise continuous, and • Remarks: • x, v not function, multiple transitions possible • q constant along continuous evolution • Can study existence uniqueness
Controller Synthesis: Example • 2D conflict resolution • Ensure aircraft remain more than 5nmi from each other
Hybrid Automaton Specification • Discrete input variable determines maneuver initiation • Safety specification
More Abstractly ... • Consider plant hybrid automaton, inputs partitioned to: • Controls, U • Disturbances, D • Controls specified by “us” • Disturbances specified by the “environment” • Unmodeled dynamics • Noise, reference signals • Actions of other agents • Memoryless controller is a map • The closed loop executions are
Controller Synthesis Problem • Given H and find g such that • A set is controlled invariant if there exists a controller such that all executions starting in remain in Proposition: The synthesis problem can be solved iff there exists a unique maximal controlled invariant set with • Seek maximal controlled invariant sets & (least restrictive) controllers that render them invariant • Proposed solution: treat the synthesis problem as a non-cooperativegame between the control and the disturbance
Gaming Synthesis Procedure • Discrete Systems: games on graphs, Bellman equation • Continuous Systems: pursuit-evasion games, Isaacs PDE • Hybrid Systems: for define • states that can be forced to jump to for some • states that may jump out of for some • states that whatever does can be continuously driven to avoiding by • Initialization: while do end
Algorithm Interpretation X Proposition: If the algorithm terminates, the fixed point is the maximal controlled invariant subset of F
Computation • One needs to compute , and • Computation of the Pre is straight forward (conceptually!): invert the transition relation • Computation of Reach through a pair of coupled Hamilton-Jacobi partial differential equations • Semi-decidable if Pre, Reach are computable • Decidable if hybrid automata are rectangular, initialized.
Entry Network • Flow optimization Link • Dynamic routing • Maneuver selection • inter-vehicle comm Coordination • Lane keeping • Vehicle following Regulation Application: Control of Automated Highway Systems • Design of vehicle controllers & performance estimation • Two concepts • platooning & individual vehicles Join Speed, vehicle following Lane Change Platoon Following Split Exit
Vehicle Following & Lane Changing • Control actions: (vehicle i) -- braking, lane change • Disturbances: (generated by neighboring vehicles) -- deceleration of the preceding vehicle -- preceding vehicle colliding with the vehicle ahead of it -- lane change resulting in a different preceding vehicles -- appearance of an obstacle in front • Operational conditions: • state of vehicle i with respect to traffic i i-1 i-2 j Computable Hybrid Systems
Game Theoretic Formulation • Requirements • Safety (no collision) • Passenger Comfort • Efficiency • trajectory tracking (depends on the maneuver) • Safe controller (J1): Solve a two-person zero-sum game • saddle solution (u1*,d1*) given by • Both vehicles i and i-1 applying maximum braking • Both collisions occur at T=0 and with maximum impact
Safe Vehicle Following Controller • Partition the state space into safe & unsafe sets • Design comfortable and • efficient controllers in • the interior • IEEE TVT 11/94 • Safe set characterization • also provides sufficient • conditions for lane change • CDC 97, CDC98
Automated Highway System Safety • Theorem 1: (Individual vehicle based AHS) • An individual vehicle based AHS can be designed to produce no inter-vehicle collisions, • moreover disturbances attenuate along the vehicle string. • Theorem 2: (Platoon based AHS) • Assuming that platoon follower operation does not result in any collisions even with a possible inter-platoon collision during join/split, a platoon based AHS can be safe under low relative velocity collision criterion. • References • Lygeros, Godbole, Sastry, IEEE TAC, April 1998 • Godbole, Lygeros, IEEE TVT, Nov. 1994
‘evader’ (control) ‘pursuer’ (disturbance) Example: Aircraft Collision Avoidance Two identical aircraft at fixed altitude & speed: y v y u x v d
y x y Continuous Reachable Set [Mitchell, Bayen, Tomlin 2001] [Tomlin, Lygeros, Sastry 2000]
Transition Systems • Transition System • Define for • Given equivalence relation define • A ~ block is a union of equivalence classes
Bisimulations of Transition Systems A partition ~ is a bisimulation iff • are ~ blocks • For all and all ~ blocks is a ~ block • Alternatively, for • Why are bisimulations important?
Bisimulation Algorithm initialize : while such that define refine • If algorithm terminates, we obtain a finite bisimulation
Computability & Finitiness • Decidability requires the bisimulation algorithm to • Terminate in finite number of steps and • Be computable • For the bisimulation algorithm to be computable we need to • Represent sets symbollically, • Perform boolean combinations on sets • Check emptyness of a set, • Compute Pre(P) of a set P • Class of sets and vector fields must be topologically simple • Set operations must not produce pathological sets • Sets must have desirable finiteness properties
Mathematical Logic • Every theory of the reals has an associated language • Decidable theories • Every formula is equivalent to a quantifier free formula • Quantifier free formulas can be decided • Quanitifier elimination • Computational tools (REDLOG, QEPCAD)
O-Minimal Theories • A definable set is • A theory of the reals is called o-minimal if every definable subset of the reals is a finite union of points and intervals • Example: for polynomial • Recent o-minimal theories Semilinear sets Semialgebraic sets Exponential flows Bounded Subanalytic sets Spirals ?
O-Minimal Hybrid Systems A hybrid system H is said to be o-minimal if • the continuous state lives in • For each discrete state, the flow of the vector field is complete • For each discrete state, all relevant sets and the flow of the vector field are definable in the same o-minimal theory Main Theorem Every o-minimal hybrid system admits a finite bisimulation. • Bisimulation alg. terminates for o-minimal hybrid systems • Various corollaries for each o-minimal theory
O-Minimal Hybrid Systems Consider hybrid systems where • All relevant sets are polyhedral • All vector fields have linear flows Then the bisimulation algorithm terminates Consider hybrid systems where • All relevant sets are semialgebraic • All vector fields have polynomial flows Then the bisimulation algorithm terminates
O-Minimal Hybrid Systems Consider hybrid systems where • All relevant sets are subanalytic • Vector fields are linear with purely imaginary eigenvalues Then the bisimulation algorithm terminates Consider hybrid systems where • All relevant sets are semialgebraic • Vector fields are linear with real eigenvalues Then the bisimulation algorithm terminates
O-Minimal Hybrid Systems Consider hybrid systems where • All relevant sets are subanalytic • Vector fields are linear with real or purely imaginary eigenvalues Then the bisimulation algorithm terminates • New o-minimal theories result in new finiteness results • Can we find constructive subclasses? • Must remain within decidable theory • Sets must be semialgebraic • Need to perfrom reachability computations • Reals with exp. does not have quantifier elimination