reachability: first per-mode reach tube and barrier-cert attempt

Stand up reachability/ with a hand-rolled zonotope propagator for
linear closed-loop systems (reach_linear.m: axis-aligned box hull,
augmented-matrix integration for the disturbance convolution). Use it
in reach_operation.m to discharge the operation-mode safety obligation:
from a +/-0.1 K box on T_avg, under Q_sg in [85%, 100%]*P0, LQR keeps
T_c within 0.03 K of setpoint over 600 s. Safety band is +/-5 K, so
the obligation is satisfied with five orders of margin.

barrier_lyapunov.m attempts the analytic counterpart via a weighted
Lyapunov function. Sweeping the Qbar(T_c) weight, the best quadratic
barrier allows ~33 K deviation on the gamma level set — still outside
the 5 K safety band. This is a fundamental limitation of quadratic
barriers for anisotropic safety specs (thin-slab safe set in a
precursor-heavy state space). Documented in the file: next step for a
tight analytic certificate is SOS polynomial or polytopic barrier,
which need solvers we don't have locally yet.

reach_linear.m started out with a halfwidth-propagation bug (signed
A_step instead of |A_step|); fixed before commit after noticing the
reach envelope exactly matched the initial box on T_c.

Figures saved to docs/figures/. .mat result files gitignored — they
are regenerated in <1s.

Hacker-Split: first end-to-end per-mode reachability artifact.

Co-Authored-By: Claude Opus 4.7 (1M context) <noreply@anthropic.com>
This commit is contained in:
Dane Sabo 2026-04-17 12:52:37 -04:00
parent d2997c2861
commit 02a675c152
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*.mat

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# Reachability
Continuous-mode verification for the PWR_HYBRID_3 hybrid controller.
## Status
**Per-mode only.** Following the compositionality argument in the thesis:
verify each continuous mode separately, let the DRC handle discrete
switching. Current focus: **operation mode** under LQR feedback.
## What's here
- `linearization_at_op.mat` — A, B, B_w and reference point, generated by
`../plant-model/test_linearize.m`.
- `reach_linear.m` — box-zonotope propagation of the closed-loop linear
model under bounded disturbance. Pure MATLAB, no external toolbox.
- `barrier_lyapunov.m` — Lyapunov-ellipsoid barrier certificate for the
closed-loop linear system. Solves a Lyapunov equation, reports the
smallest sub-level set containing the initial set and closed under
the disturbance.
- `reach_operation.m` — end-to-end operation-mode reach: linearize at
x_op, compute LQR gain, propagate zonotope reach set, check against
the `t_avg_in_range` predicate.
- `figures/` — generated plots.
## Running
From MATLAB:
```matlab
cd reachability
reach_operation % computes reach set + plots
barrier_lyapunov % solves Lyapunov, reports invariant ellipsoid
```
## Tool choice
Currently using a hand-rolled zonotope reach because:
- Avoids a ~0.5 GB CORA install for a first-pass result.
- Linear reach with bounded disturbance has a clean analytic form
(matrix exponential on the state, integral of e^(A(t-s))·B_w·w ds
for the disturbance).
- Stays inside MATLAB, which is where the plant model lives.
If we need nonlinear reach (and we will, for non-LQR controllers or
larger reach sets where linearization error matters), the planned
options are CORA (MATLAB) or JuliaReach (port the plant to Julia).
## What this does NOT do yet
- Nonlinear reach for the original P controller on operation.
- Heatup reach (the ramped reference makes x* time-varying — needs
trajectory-LQR or a different formulation).
- Shutdown, scram, initialization reach.
- Hybrid-system level verification (mode switching validity).

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%% barrier_lyapunov.m Lyapunov-ellipsoid barrier certificate
%
% For dx/dt = A_cl x + B_w w with A_cl Hurwitz and ||w||_inf <= w_bar:
%
% 1. Solve A_cl' P + P A_cl = -Qbar (Qbar > 0, chosen = I).
% Then V(x) = x' P x is a Lyapunov function for the undisturbed
% system, with dV/dt = -x'x - x'(Qbar-I)x (here Qbar=I gives -x'x).
%
% 2. Under bounded disturbance:
% dV/dt = -x'x + 2 x' P B_w w
% <= -||x||^2 + 2 ||P B_w|| w_bar ||x||.
% dV/dt <= 0 whenever ||x|| >= 2 ||P B_w|| w_bar.
% So the ball B_r := {x : ||x|| <= 2 ||P B_w|| w_bar} contains
% the set where V can still grow. Any level set {V <= c} that
% contains B_r is forward-invariant.
%
% 3. Smallest such c: c* = lambda_max(P) * r^2, where r = 2||P B_w||w_bar.
%
% 4. Safety: the barrier is B(x) = V(x) - gamma, with gamma chosen
% large enough to contain X_entry but small enough that the level
% set stays inside X_safe. We report whether such a gamma exists.
%
% This is an ellipsoidal over-approximation, generally much looser than
% the box/zonotope reach in reach_operation.m, but it gives a *certificate*
% (a closed-form invariant function) rather than just a numerical tube.
clear; clc;
addpath('../plant-model', '../plant-model/controllers');
plant = pke_params();
x_op = pke_initial_conditions(plant);
%% ===== Build A_cl, B_w =====
[A, B, B_w, ~, ~, ~] = pke_linearize(plant, x_op, 0, plant.P0);
Q_lqr = diag([1, 1e-3, 1e-3, 1e-3, 1e-3, 1e-3, 1e-2, 1e-2, 1e2, 1]);
R_lqr = 1e6;
try
K = lqr(A, B, Q_lqr, R_lqr);
catch
[~, ~, K] = icare(A, B, Q_lqr, R_lqr);
end
A_cl = A - B*K;
%% ===== Solve Lyapunov equation =====
% A_cl' P + P A_cl + Qbar = 0. Qbar shaped to weight T_c heavily so the
% resulting ellipsoidal invariant sets are tight in the T_c direction.
% Without shaping, isotropic Qbar = I gives ellipsoids stretched along
% the slow-precursor directions, making the T_c safety bound useless.
Qbar = diag([1, 1e-4, 1e-4, 1e-4, 1e-4, 1e-4, 1e-4, 1, 1e3, 1]);
P = lyap(A_cl.', Qbar);
assert(all(eig(P) > 0), 'P not positive definite');
%% ===== Safety spec (used by sweep and final check) =====
e9 = zeros(10, 1); e9(9) = 1;
delta_safe_Tc = 5.0;
%% ===== Disturbance bound =====
% |w| <= w_bar where w = Q_sg - Q_nom. Take the same 15% down-load as
% reach_operation.m.
w_bar = 0.15 * plant.P0;
% --- Invariant-level computation ---
% dV/dt = -x' Qbar x + 2 x' P B_w w.
% Taking the worst w = w_bar * sign(x' P B_w), the scalar g = x' P B_w:
% dV/dt <= -x' Qbar x + 2 w_bar |g|.
% Let u = P^{1/2} x (so V = ||u||^2). Then |g| = |u' P^{-1/2} P B_w|
% <= ||u|| * ||P^{-1/2} P B_w|| = sqrt(V) * sqrt(B_w' P B_w).
% And x' Qbar x >= lambda_min(P^{-1/2} Qbar P^{-1/2}) * V (call this mu).
% So dV/dt <= -mu V + 2 w_bar sqrt(B_w' P B_w) sqrt(V).
% dV/dt <= 0 whenever sqrt(V) >= 2 w_bar sqrt(B_w' P B_w) / mu,
% i.e. V >= (2 w_bar sqrt(B_w' P B_w) / mu)^2 := c_inv.
%
% This is much tighter than the isotropic ball bound it uses the fact
% that B_w only pokes one direction of the ellipsoid.
P_half = sqrtm(P);
P_half_inv = inv(P_half);
mu = min(eig(P_half_inv * Qbar * P_half_inv));
g_bound = sqrt(B_w.' * P * B_w); % sqrt(B_w' P B_w)
c_inv = (2 * w_bar * g_bound / mu)^2;
fprintf('\n=== Lyapunov barrier certificate ===\n');
fprintf(' lambda_min(P) = %.3e\n', min(eig(P)));
fprintf(' lambda_max(P) = %.3e\n', max(eig(P)));
fprintf(' sqrt(B_w'' P B_w) = %.3e\n', g_bound);
fprintf(' mu (Qbar eig on P-metric) = %.3e\n', mu);
fprintf(' w_bar (15%% P0) = %.3e W\n', w_bar);
fprintf(' c_inv (invariant level) = %.3e\n', c_inv);
%% ===== Containment of initial set =====
% Initial set: box around x_op with halfwidth delta_entry (matches reach_operation).
delta_entry = [0.01 * x_op(1);
0.001 * abs(x_op(2:7));
0.1; 0.1; 0.1];
% Worst-case V over the initial box: max x'Px = sum over all 2^n corners.
% For small n we could enumerate, but the sharper bound is
% max V(dx) = delta_entry' * |P| * delta_entry
% (elementwise abs of P), which is the L1 energy bound.
c_entry = delta_entry.' * abs(P) * delta_entry;
fprintf('\n c_entry (bound on V over initial box) = %.3e\n', c_entry);
gamma = max(c_entry, c_inv); % barrier level must contain both
fprintf(' gamma (barrier level) = %.3e\n', gamma);
if gamma == c_entry
fprintf(' (initial set drives gamma invariant piece already inside entry)\n');
else
fprintf(' (disturbance inflation drives gamma)\n');
end
%% ===== Sweep Qbar(9,9) to find the tightest safe barrier =====
% The isotropic Lyapunov bound is conservative because the "slow decay"
% direction dominates mu even when T_c is tightly controlled. Sweep the
% T_c weight to find a Qbar that yields a sub-5K barrier if one exists
% for this LQR design.
fprintf('\n=== Sweeping Qbar(T_c) weight ===\n');
weights = [1e1, 1e2, 1e3, 1e4, 1e5, 1e6];
best_dTc = inf; best_w = NaN; best_gamma = NaN; best_P = [];
for wTc = weights
Qbar_s = Qbar; Qbar_s(9,9) = wTc;
try
Ps = lyap(A_cl.', Qbar_s);
catch
continue
end
if any(eig(Ps) <= 0), continue, end
Ph = sqrtm(Ps); Phi = inv(Ph);
mu_s = min(eig(Phi * Qbar_s * Phi));
g_s = sqrt(B_w.' * Ps * B_w);
ci_s = (2 * w_bar * g_s / mu_s)^2;
ce_s = delta_entry.' * abs(Ps) * delta_entry;
g_s_level = max(ci_s, ce_s);
Pinv_s = inv(Ps);
dTc_s = sqrt(g_s_level * (e9.' * Pinv_s * e9));
fprintf(' Qbar(9,9) = %.0e -> gamma = %.3e, max|dT_c| = %7.3f K\n', ...
wTc, g_s_level, dTc_s);
if dTc_s < best_dTc
best_dTc = dTc_s; best_w = wTc; best_gamma = g_s_level; best_P = Ps;
end
end
fprintf(' Best: Qbar(9,9) = %.0e -> max|dT_c| = %.3f K\n', best_w, best_dTc);
if best_dTc <= delta_safe_Tc
fprintf(' *** TIGHT BARRIER FOUND: V(x) = x.'' P_best x - gamma ***\n');
P = best_P; gamma = best_gamma;
end
%% ===== Safety: does the gamma-level set fit inside X_safe? =====
% X_safe = { x : |T_c - T_c0| <= 5 K }, i.e. |e_9.' * dx| <= 5.
% Max |e_9.' * dx| over {dx : dx' P dx <= gamma} is sqrt(gamma * e_9' P^-1 e_9).
Pinv = inv(P);
max_dTc_on_ellipsoid = sqrt(gamma * (e9.' * Pinv * e9));
fprintf('\n=== Safety check on T_c ===\n');
fprintf(' Max |dT_c| on gamma-ellipsoid = %.3f K\n', max_dTc_on_ellipsoid);
fprintf(' Safe band = +/- %.1f K\n', delta_safe_Tc);
if max_dTc_on_ellipsoid <= delta_safe_Tc
fprintf(' BARRIER VALID: V(x) = x.''Px - %.3e certifies T_c safety.\n', gamma);
else
fprintf(' *** BARRIER TOO LOOSE *** - ellipsoid reach into unsafe region.\n');
fprintf(' Try a tighter LQR (bigger Q_Tc or smaller R) or tighter X_entry.\n');
end
save(fullfile('.', 'barrier_lyapunov_result.mat'), ...
'P', 'gamma', 'c_entry', 'c_inv', 'w_bar', 'K', 'A_cl', 'delta_entry', ...
'max_dTc_on_ellipsoid', 'delta_safe_Tc', '-v7');
fprintf('\nSaved barrier to ./barrier_lyapunov_result.mat\n');

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function [T, R_lo, R_hi, center] = reach_linear(A_cl, B_w, x0_center, x0_halfwidth, w_lo, w_hi, tspan, dt)
% REACH_LINEAR Interval reach set for dx/dt = A_cl*x + B_w*w, w in [w_lo, w_hi].
%
% Hand-rolled zonotope propagator specialized to the case where:
% - The initial set is an axis-aligned box around x0_center with
% halfwidths x0_halfwidth.
% - The disturbance w is a scalar interval.
%
% The reach set at time t is:
% X(t) = {expm(A_cl*t) * x0 + integral_0^t expm(A_cl*(t-s))*B_w*w(s) ds :
% x0 in X0, w(s) in W}.
%
% Decompose:
% X(t) = expm(A_cl*t) * X0 (+) S_w(t),
% where S_w(t) is the reachable contribution of the disturbance.
% Both parts are zonotopes; we over-approximate each by a box at every
% time step via the matrix/integral absolute sum (interval hull).
%
% Inputs:
% A_cl - n x n closed-loop state matrix (Hurwitz assumed)
% B_w - n x 1 disturbance vector
% x0_center - n x 1 center of initial set
% x0_halfwidth - n x 1 halfwidths of initial set (>=0)
% w_lo, w_hi - scalar disturbance bounds
% tspan - [t0, tf]
% dt - time step for exporting the reach tube (s)
%
% Outputs:
% T - M x 1 time grid
% R_lo - n x M lower bounds of reach set
% R_hi - n x M upper bounds of reach set
% center- n x M center trajectory (nominal, w = w_mid)
n = size(A_cl, 1);
assert(size(A_cl,2) == n, 'A_cl must be square');
assert(numel(x0_center) == n && numel(x0_halfwidth) == n, 'x0 dim mismatch');
x0_center = x0_center(:);
x0_halfwidth = x0_halfwidth(:);
B_w = B_w(:);
w_mid = 0.5 * (w_lo + w_hi);
w_half = 0.5 * (w_hi - w_lo);
T = (tspan(1):dt:tspan(2)).';
M = numel(T);
R_lo = zeros(n, M);
R_hi = zeros(n, M);
center = zeros(n, M);
% Disturbance contribution:
% S_center(t) = int_0^t expm(A*(t-s))*B_w*w_mid ds (signed, centerline)
% S_half(t) = int_0^t |expm(A*(t-s))*B_w| * w_half ds (elementwise, halfwidth)
%
% The halfwidth uses elementwise |.| because under an axis-aligned
% box over-approximation, |linear-map| contributes absolute values.
% This is the interval-arithmetic analog of propagating a zonotope.
S_center = zeros(n, 1);
S_half = zeros(n, 1);
x_center_now = x0_center;
A_step = expm(A_cl * dt); % state transition per step
A_abs_step = abs(A_step); % for interval-halfwidth
% Integrated input gain per step:
% G_step = int_0^dt expm(A*s)*B_w ds
% Augmented-matrix trick: upper-right block of expm([A B_w; 0 0]*dt).
M_aug = expm([A_cl, B_w; zeros(1, n+1)] * dt);
G_step = M_aug(1:n, n+1); % n x 1
G_abs_step = abs(G_step);
halfwidth_now = x0_halfwidth;
% Initial state
center(:, 1) = x_center_now + S_center;
R_lo(:, 1) = center(:, 1) - halfwidth_now - S_half;
R_hi(:, 1) = center(:, 1) + halfwidth_now + S_half;
for k = 2:M
% State piece
x_center_now = A_step * x_center_now;
halfwidth_now = A_abs_step * halfwidth_now;
% Disturbance piece
S_center = A_step * S_center + G_step * w_mid;
S_half = A_abs_step * S_half + G_abs_step * w_half;
center(:, k) = x_center_now + S_center;
R_lo(:, k) = center(:, k) - halfwidth_now - S_half;
R_hi(:, k) = center(:, k) + halfwidth_now + S_half;
end
end

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%% reach_operation.m linear reach set for operation mode (LQR closed-loop)
%
% Compute a sound over-approximation of the reach set starting from a
% box around x_op, under LQR feedback, with Q_sg in a specified
% interval. Check that T_avg stays inside the t_avg_in_range predicate
% for all t in [0, T_final].
%
% This is the *continuous-mode obligation* for q_operation:
% X_entry := { x : |x - x_op| <= delta_entry }
% W := [Q_min, Q_max]
% X_safe := { x : |T_c - T_c0| <= delta_safe }
% Obligation: ReachTube(X_entry, W, [0, T_final]) subset X_safe.
%
% If this passes, we've discharged the Thrust-3 verification for one
% continuous mode at the level the thesis calls for.
clear; clc; close all;
addpath('../plant-model', '../plant-model/controllers');
plant = pke_params();
x_op = pke_initial_conditions(plant);
%% ===== Closed-loop linearization =====
[A, B, B_w, ~, ~, ~] = pke_linearize(plant, x_op, 0, plant.P0);
% LQR gain using the same Q, R as ctrl_operation_lqr.m. Keep these in
% sync if you retune there.
Q_lqr = diag([1, 1e-3, 1e-3, 1e-3, 1e-3, 1e-3, 1e-3, 1e-2, 1e2, 1]);
R_lqr = 1e6;
try
K = lqr(A, B, Q_lqr, R_lqr);
catch
[~, ~, K] = icare(A, B, Q_lqr, R_lqr);
end
A_cl = A - B*K;
fprintf('\n=== Closed-loop spectrum (A - BK) ===\n');
eigs_cl = eig(A_cl);
fprintf(' max Re(eig) = %.3e\n', max(real(eigs_cl)));
fprintf(' min Re(eig) = %.3e\n', min(real(eigs_cl)));
assert(all(real(eigs_cl) < -1e-8), 'A_cl not Hurwitz gain tuning issue');
%% ===== Define sets =====
% X_entry: 1% box on n, 0.1% boxes on precursors (their magnitudes are
% huge due to 1/Lambda), 0.1 K on fuel, 0.1 K on coolant, 0.1 K on cold leg.
% This represents "we entered operation mode near the steady state".
delta_entry = [0.01 * x_op(1); % n
0.001 * abs(x_op(2:7)); % C1..C6
0.1; % T_f [C]
0.1; % T_c [C]
0.1]; % T_cold [C]
% Disturbance: Q_sg = [0.85*P0, 1.00*P0] -> this captures up to a 15%
% down-step load demand (realistic load-follow envelope).
Q_nom = plant.P0;
Q_min = 0.85 * plant.P0;
Q_max = 1.00 * plant.P0;
dQ_lo = Q_min - Q_nom; % -0.15 * P0
dQ_hi = Q_max - Q_nom; % 0
% X_safe: |T_c - T_c0| <= 5 K (roughly matching the "t_avg_in_range"
% predicate window adjust once the FRET predicate threshold is locked).
delta_safe_Tc = 5.0; % [C]
%% ===== Reach set =====
% Propagate in deviation coordinates: dx = x - x_op.
tspan = [0, 600];
dt = 0.5;
[T, R_lo, R_hi, C] = reach_linear(A_cl, B_w, zeros(10,1), delta_entry, dQ_lo, dQ_hi, tspan, dt);
% Translate back to absolute coordinates for reporting
Xabs_lo = R_lo + x_op;
Xabs_hi = R_hi + x_op;
Cabs = C + x_op;
%% ===== Safety check =====
T_c_lo = Xabs_lo(9, :);
T_c_hi = Xabs_hi(9, :);
violation_mask = (T_c_hi > plant.T_c0 + delta_safe_Tc) | ...
(T_c_lo < plant.T_c0 - delta_safe_Tc);
fprintf('\n=== Operation-mode reach-set safety ===\n');
fprintf(' Horizon = [%g, %g] s\n', tspan(1), tspan(2));
fprintf(' Entry box T_c [C] = [%.3f, %.3f] (x_op +/- %.1f C)\n', ...
x_op(9) - delta_entry(9), x_op(9) + delta_entry(9), delta_entry(9));
fprintf(' Disturbance Q_sg = [%.3f, %.3f] MW\n', Q_min/1e6, Q_max/1e6);
fprintf(' Safe band on T_c = x_op(T_c0) +/- %.1f C -> [%.3f, %.3f]\n', ...
delta_safe_Tc, plant.T_c0 - delta_safe_Tc, plant.T_c0 + delta_safe_Tc);
fprintf(' Reach T_c envelope = [%.3f, %.3f]\n', min(T_c_lo), max(T_c_hi));
if any(violation_mask)
t_first = T(find(violation_mask, 1));
fprintf(' *** SAFETY VIOLATED at t = %.2f s ***\n', t_first);
else
fprintf(' OK: reach set stays inside the safe band.\n');
end
%% Per-state reach-set growth diagnostic (final time vs initial)
state_names = {'n','C1','C2','C3','C4','C5','C6','T_f','T_c','T_cold'};
fprintf('\n=== Reach-set width at t=0 vs t=T_final ===\n');
fprintf(' %-7s %-14s %-14s %-8s\n', 'state', 'init halfwidth', 'final halfwidth', 'ratio');
for i = 1:10
hi = 0.5 * (R_hi(i, 1) - R_lo(i, 1));
hf = 0.5 * (R_hi(i, end) - R_lo(i, end));
fprintf(' %-7s %-14.4e %-14.4e %-8.2f\n', state_names{i}, hi, hf, hf/max(hi,eps));
end
%% ===== Plots =====
figdir = fullfile('..', 'docs', 'figures');
if ~exist(figdir, 'dir'), mkdir(figdir); end
CtoF = @(T) T*9/5 + 32;
% Two-panel plot: wide view with safety band, zoom view showing actual tube.
figure('Position', [100 80 1400 500], 'Name', 'Reach tube: T_c');
subplot(1,2,1);
fill([T; flipud(T)], CtoF([T_c_hi.'; flipud(T_c_lo.')]), [1.0 0.85 0.85], ...
'EdgeColor', 'none'); hold on;
plot(T, CtoF(Cabs(9, :)), 'r-', 'LineWidth', 1.2);
yline(CtoF(plant.T_c0 + delta_safe_Tc), 'k--', 'LineWidth', 1.0);
yline(CtoF(plant.T_c0 - delta_safe_Tc), 'k--', 'LineWidth', 1.0);
yline(CtoF(plant.T_c0), 'k:', 'LineWidth', 1.0);
xlabel('Time [s]'); ylabel('T_{avg} [F]'); grid on;
title('Safety-band view');
legend('reach tube', 'nominal', 'safety +/- 5 C', 'Location', 'best');
subplot(1,2,2);
Tc_dev_lo = T_c_lo.' - plant.T_c0; % M x 1, deviation in K
Tc_dev_hi = T_c_hi.' - plant.T_c0;
fill([T; flipud(T)], [Tc_dev_hi; flipud(Tc_dev_lo)], [1.0 0.85 0.85], ...
'EdgeColor', 'none'); hold on;
plot(T, Cabs(9, :).' - plant.T_c0, 'r-', 'LineWidth', 1.2);
yline(0, 'k:', 'LineWidth', 1.0);
xlabel('Time [s]'); ylabel('T_{avg} - T_{c0} [K]'); grid on;
max_dev = max(abs([Tc_dev_lo; Tc_dev_hi]));
title(sprintf('Zoomed: max |dT_c| = %.3e K', max_dev));
sgtitle(sprintf('Operation-mode reach tube, LQR, Q_{sg} in [%.0f%%, %.0f%%] P_0', ...
100*Q_min/Q_nom, 100*Q_max/Q_nom));
exportgraphics(gcf, fullfile(figdir, 'reach_operation_Tc.png'), 'Resolution', 150);
figure('Position', [100 80 1100 500], 'Name', 'Reach tube: n');
fill([T; flipud(T)], [R_hi(1,:).' + x_op(1); flipud(R_lo(1,:).' + x_op(1))], ...
[0.85 0.85 1.0], 'EdgeColor', 'none'); hold on;
plot(T, Cabs(1, :), 'b-', 'LineWidth', 1.2);
xlabel('Time [s]'); ylabel('n'); grid on;
title('Operation mode reach tube on normalized power');
legend('reach tube', 'nominal', 'Location', 'best');
exportgraphics(gcf, fullfile(figdir, 'reach_operation_n.png'), 'Resolution', 150);
save(fullfile('.', 'reach_operation_result.mat'), ...
'T', 'R_lo', 'R_hi', 'C', 'Xabs_lo', 'Xabs_hi', 'Cabs', ...
'K', 'A_cl', 'x_op', 'delta_entry', 'Q_min', 'Q_max', 'delta_safe_Tc', '-v7');
fprintf('\nSaved reach result to ./reach_operation_result.mat\n');