trajectory-based-controlled-invariants

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Compute controlled invariant sets for linear discrete-time systems using trajectory-based approach with convex feasible points. Use for MPC design, control invariant set computation, feasibility guarantees, and discrete-time system analysis. Keywords: controlled invariant, MPC, trajectory-based, convex feasible points, discrete-time systems, recursive feasibility.

hiyenwong By hiyenwong schedule Updated 6/3/2026

name: trajectory-based-controlled-invariants description: "Compute controlled invariant sets for linear discrete-time systems using trajectory-based approach with convex feasible points. Use for MPC design, control invariant set computation, feasibility guarantees, and discrete-time system analysis. Keywords: controlled invariant, MPC, trajectory-based, convex feasible points, discrete-time systems, recursive feasibility."

Trajectory-Based Controlled Invariants

Description

A trajectory-based approach to computing controlled invariant sets for linear discrete-time systems. Introduces convex feasible points concept for invariant set characterization and provides MPC schemes with recursive feasibility guarantees without precomputed terminal sets.

Activation Keywords

  • controlled invariant
  • controlled invariant set
  • trajectory-based invariants
  • convex feasible points
  • MPC recursive feasibility
  • discrete-time system invariance
  • 控制不变集
  • MPC 可行性
  • 轨迹方法不变集

Tools Used

  • exec: Run Python scripts for system analysis
  • read: Load system models, reference papers
  • write: Save invariant set computations

Core Concepts

1. Convex Feisible Points

Definition: A finitely long state trajectory that provides new characterization of controlled invariance.

Key Properties:

  • Provides necessary condition for control invariance
  • Can be verified with finite trajectory length
  • Combines with backward fixed-point algorithm

2. Controlled Invariant Sets

Sets where system state can remain indefinitely under proper control.

Traditional Methods:

  • Backward reachability
  • Fixed-point iteration

Trajectory-Based Innovation:

  • Uses finite trajectories instead of infinite analysis
  • Reduces computational complexity
  • Enables practical MPC design

3. MPC without Terminal Sets

Two proposed MPC schemes:

  1. Direct feasibility guarantee via trajectory constraints
  2. Recursive feasibility through convex feasible points

Advantages:

  • No need for precomputed terminal sets
  • Online feasibility verification
  • Reduced offline computation burden

Instructions for Agents

Step 1: System Modeling

Given discrete-time linear system:

x(k+1) = Ax(k) + Bu(k)

Identify:

  • State matrix A
  • Input matrix B
  • State constraints X
  • Input constraints U

Step 2: Trajectory Analysis

  1. Generate candidate trajectories
  2. Verify convex feasible point conditions
  3. Check trajectory constraints satisfaction

Verification criterion:

  • Trajectory must remain in X for all steps
  • Control inputs must satisfy U constraints
  • Must provide convex hull feasible for continuation

Step 3: Invariant Set Computation

Use backward fixed-point algorithm:

def compute_maximal_invariant(A, B, X, U, iterations=100):
    """Compute maximal controlled invariant set."""
    current_set = X
    for i in range(iterations):
        # Backward reachable set
        predecessor = backward_reach(A, B, current_set, U)
        # Intersection with constraints
        current_set = predecessor ∩ X
        if current_set.is_empty():
            break
    return current_set

Step 4: MPC Design

Construct MPC scheme:

def mpc_trajectory_based(x_current, horizon, A, B, X, U, convex_feasible_point):
    """MPC with trajectory-based feasibility guarantee."""
    # Optimization problem
    # Variables: x(0:N), u(0:N-1)
    # Constraints:
    #   - Dynamics: x(k+1) = Ax(k) + Bu(k)
    #   - State: x(k) ∈ X
    #   - Input: u(k) ∈ U
    #   - Feasibility: convex_feasible_point condition
    # Objective: minimize cost function
    
    return optimal_sequence

Step 5: Feasibility Verification

Check recursive feasibility:

  • Verify convex feasible point at each iteration
  • Ensure existence of feasible continuation
  • Validate constraint satisfaction

Use Cases

Use Case 1: Safety-Critical Control

Scenario: Robot navigation with obstacle avoidance

Application:

  • Define safety constraints (avoid obstacles)
  • Compute controlled invariant safe set
  • Design MPC guaranteeing perpetual safety
  • No precomputation of terminal safe set needed

Use Case 2: Resource Management

Scenario: Tank level control with limits

Application:

  • State constraints: tank level bounds
  • Input constraints: pump capacity
  • Compute invariant operating region
  • MPC maintains feasibility indefinitely

Use Case 3: Power System Control

Scenario: Generator scheduling with stability constraints

Application:

  • State: power output, frequency
  • Input: control signals
  • Invariant set ensures stability
  • Trajectory-based simplifies computation

Mathematical Formulation

Convex Feisible Point Definition

A trajectory {x(0), x(1), ..., x(N)} is a convex feasible point if:

  1. State constraints: x(k) ∈ X for all k
  2. Input constraints: u(k) ∈ U satisfies x(k+1) = Ax(k) + Bu(k)
  3. Convexity: There exists convex combination enabling continuation

Optimization Problem

minimize   Σ J(x(k), u(k))
subject to x(k+1) = Ax(k) + Bu(k), k = 0, ..., N-1
           x(k) ∈ X, k = 0, ..., N
           u(k) ∈ U, k = 0, ..., N-1
           convex_feasible_point(x(N)) = true

Error Handling

Infeasible Initial State

Problem: Current state outside invariant set

Solution:

  • Check feasibility before MPC execution
  • If infeasible, use recovery maneuver
  • Plan trajectory to invariant set boundary

Invariant Set Computation Failure

Problem: Algorithm doesn't converge

Solution:

  • Increase iteration limit
  • Check constraint compatibility
  • Verify system controllability
  • Adjust numerical precision

Numerical Issues

Problem: Convex hull computation unstable

Solution:

  • Use robust convex hull algorithms
  • Increase trajectory length
  • Apply regularization techniques

Examples

Example 1: Double Integrator

System:

A = [[1, 1], [0, 1]]
B = [[0], [1]]
X = {x: |x₁| ≤ 10, |x₂| ≤ 2}
U = {u: |u| ≤ 1}

Process:

  1. Generate trajectories with N=10
  2. Identify convex feasible points
  3. Compute maximal invariant set
  4. Design MPC with horizon 5

Example 2: Room Temperature Control

System:

A = 0.95  # Decay rate
B = 1.0   # Heating effect
X = [18°C, 25°C]
U = [0kW, 5kW]

Application:

  • Compute temperature invariant interval
  • MPC maintains comfortable temperature
  • No terminal set precomputation

Resources

  • Paper: arXiv:2604.07225 - "A Trajectory-based Approach to Controlled Invariants"
  • Code: scripts/compute_invariant_set.py
  • References: references/discrete_time_control.md

Related Skills

  • kuramoto-control-theory: Synchronization control
  • robust-regret-control: Robust MPC design
  • ml-complexity-management: Complexity analysis for control

Notes

  • Applicable to linear discrete-time systems only
  • Numerical stability depends on trajectory length
  • Convexity assumption required
  • MPC horizon affects computational load
Install via CLI
npx skills add https://github.com/hiyenwong/ai_collection --skill trajectory-based-controlled-invariants
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