# Pitch Bandwidth Criteria > Use when you must assess the pitch-axis flying qualities of an aircraft with the MIL-STD-1797A bandwidth and phase-delay criterion: model the pitch attitude response as a short period transfer function with a control anticipation numerator time constant and an actuator lag, evaluate the frequency response, find the bandwidth frequency omega_BW as the lower of the 45 degree phase margin frequency and the 6 dB gain margin frequency, read the -180 degree frequency, compute the phase delay tau_p from the phase at twice omega_180, and grade the Category A Level 1, 2 and 3 boundaries. Produces omega_BW, omega_180, tau_p, the flying qualities level and the limiting criterion. Trigger: pitch bandwidth criterion, phase delay tau, bandwidth frequency, phase margin 45 degrees, mil-std-1797a bandwidth, short period transfer function, actuator lag, flying qualities level. - Skill: `ashfordeou/pitch-bandwidth-criteria` (Agent Skill, multi-file: 3 files) - Install (CLI): `npx skillmds@latest add ashfordeou/pitch-bandwidth-criteria` - Raw SKILL.md: https://api.skillmd.com/api/skills/ashfordeou/pitch-bandwidth-criteria/raw - Safety review: pending - Works with: Claude Code, Claude.ai, OpenAI Codex - Category: AI & ML - License: Apache-2.0 - Author: ashfordeOU (https://skillmd.com/u/ashfordeou) - Updated: 2026-09-17 - Page: https://skillmd.com/skills/ashfordeou/pitch-bandwidth-criteria --- # Pitch Bandwidth Criteria (flight-mechanics/handling-qualities/pitch-bandwidth-criteria) Use when the task is assessing pitch-axis flying qualities with the MIL-STD-1797A bandwidth and phase-delay criterion, the frequency-domain method that grades the pitch attitude response directly from its open loop frequency response. This leaf models the pitch attitude transfer function as a short period mode plus a control anticipation numerator time constant and an actuator lag, evaluates the response, extracts the bandwidth frequency omega_BW and the phase delay tau_p, and returns the Level 1, 2 or 3 verdict with the limiting criterion. It is the companion to the modal level tables in the mil-std-1797a leaf: same standard, different assessment method (frequency-domain bandwidth instead of per-mode damping tables). Implementation is pure Python, stdlib only, deterministic and offline. ## Domain quick reference - Pitch attitude model (K normalized to 1.0, the criterion uses phase and gain ratio only): G(s) = (1 + T_th2*s) / (s * (s^2 + 2*zeta*wn*s + wn^2) * (1 + s/w_act)), with wn the short period natural frequency (rad/s), zeta the short period damping, T_th2 the control anticipation time constant (s) and w_act the actuator lag frequency (rad/s). - Unwrapped phase: phase = atan(w*T_th2) - 90 - atan2(2*zeta*wn*w, wn^2 - w^2) - atan(w/w_act) degrees, continuous from -90 degrees at the origin (the lead term can lift it a fraction of a degree just above zero before the mode lag dominates). The module unwraps the principal phase numerically over a fine 0.01 rad/s grid and refines every crossing with a bisection root finder. - Bandwidth definition: omega_BW is the lower of the frequency at which the phase margin is 45 degrees (phase equals -135 degrees, omega_135) and the 6 dB gain margin frequency (omega_GM6). A -6 dB gain crossing counts only when it sits at or beyond the -180 degree phase crossing, the region where gain margin actually limits the loop; the low frequency crossing of the normalized response (phase near -93 degrees) never limits bandwidth and is reported as None. Documented assumption of this leaf, recorded because the gain is normalized to unity. - Phase delay: tau_p = -(phase(2*omega_180) + 180) / (2*omega_180) * (pi/180) seconds, from the unwrapped phase at twice the -180 degree frequency. None when omega_180 does not exist. - Level boundaries (representative Category A pitch values from MIL-STD-1797A 4.5.1, class dependent in the standard; verify against the current revision before certifying an airframe): Level 1 needs omega_BW >= 3.5 rad/s and tau_p <= 0.2 s; Level 2 needs omega_BW >= 2.5 rad/s and tau_p <= 0.2 s; otherwise Level 3. The limiting criterion is bandwidth, phase delay or both. - ValueErrors: wn <= 0, zeta <= 0 or >= 1, T_th2 <= 0, w_act <= wn, and a non-positive evaluation frequency are rejected. ## Workflow 1. Fix the airframe response parameters: short period wn and zeta (from the stability leaves or a flight test short period fit), the control anticipation time constant T_th2 and the actuator lag frequency w_act. Check that w_act > wn. 2. Evaluate the criterion metrics with bandwidth(wn, zeta, T_th2, w_act): it returns omega_135, omega_GM6, omega_BW, omega_180 and tau_p. The unwrapped phase comes from phase_deg and the magnitude from mag_db; crossings are located by find_root_phase over the dense unwrapped phase table with bisection refinement. 3. Grade the result with level_verdict(omega_BW, tau_p), which returns the level, the limiting criterion (bandwidth, phase delay or both) and any metric that could not be computed. Verify the numerical building blocks separately when needed: transfer for the complex response and unwrap_phase_deg for phase series continuity. 4. State the verdict with the governing metric. When the level boundaries sit near the computed values, recheck the aircraft class and flight phase category against the current MIL-STD-1797A revision because the representative boundaries used here are Category A values and are class dependent. 5. Confirm the deterministic checks with the contract test scripts/test_pitch_bandwidth_criteria.py. ## Worked example Case A: wn = 4.0 rad/s, zeta = 0.7, T_th2 = 0.5 s, w_act = 25 rad/s. - omega_135 = 4.58 rad/s: the 45 degree phase margin crossing. The 6 dB gain margin crossing is not reached in the stability relevant band (omega_GM6 is None), so omega_BW = omega_135 = 4.58 rad/s. - omega_180 = 10.13 rad/s; the phase at twice omega_180 gives tau_p = 0.0247 s. - Verdict: Level 1 (omega_BW 4.58 >= 3.5 and tau_p 0.0247 <= 0.2), limiting criterion bandwidth. Case B: wn = 3.0 rad/s, zeta = 0.6, T_th2 = 0.7 s, w_act = 20 rad/s. - omega_135 = 3.43 rad/s, omega_BW = 3.43 rad/s, omega_180 = 7.23 rad/s, tau_p = 0.0325 s. - Verdict: Level 2 (omega_BW 3.43 is below the Level 1 floor of 3.5 but above 2.5; tau_p is fine), limiting criterion bandwidth. ## Verification - bandwidth(4.0, 0.7, 0.5, 25.0) returns omega_135 4.5832 rad/s, omega_180 10.1290 rad/s, tau_p 0.0246 s, omega_GM6 None and omega_BW equal to omega_135; level_verdict gives Level 1, limiting bandwidth. - bandwidth(3.0, 0.6, 0.7, 20.0) returns omega_135 3.4315 rad/s, omega_180 7.2257 rad/s, tau_p 0.0325 s and a Level 2 verdict. - Confirm the lightly damped trend: at zeta 0.35 the phase drops faster and omega_135 is below the zeta 0.7 value at the same wn. - Confirm every non-positive wn and w, zeta outside (0, 1), T_th2 <= 0 and w_act <= wn raises ValueError. - Run the contract test offline: python3 scripts/test_pitch_bandwidth_criteria.py (35 tests, deterministic, passes in under a second). ## Pitfalls - Treating the level boundaries as universal: the 3.5/2.5 rad/s bandwidth floors and 0.2 s phase-delay limit are representative Category A values and are class dependent in MIL-STD-1797A; recheck class and category against the current revision before a certification-grade verdict, especially when the computed metrics sit near a boundary. - Reading omega_GM6 = None as zero: the -6 dB gain crossing counts only when it sits at or beyond the -180 degree crossing; the low-frequency crossing of the normalized response never limits bandwidth and is reported None, so None means 'not bandwidth limiting', not a 0 rad/s limit. - Computing tau_p without omega_180: the phase delay is read from the unwrapped phase at twice the -180 degree frequency and is None when omega_180 does not exist; evaluating the formula at an arbitrary frequency gives a meaningless number. - Ignoring the w_act > wn constraint: an actuator lag at or below the short period frequency is rejected (ValueError), and a marginally separated w_act distorts the high-frequency phase that sets omega_180 and tau_p. - Trusting principal phase without unwrapping: crossings are located on the numerically unwrapped phase table with bisection refinement; wrapping artifacts around -180 degrees would shift omega_180 and the phase delay. ## Related leaves - flight-mechanics/handling-qualities/mil-std-1797a: the modal level table companion criterion from the same standard; this leaf applies the frequency-domain bandwidth method instead of the per-mode tables. - flight-mechanics/handling-qualities/pilot-induced-oscillation: phase-related neighbor for pilot-in-the-loop coupling risk. - flight-mechanics/handling-qualities/cooper-harper-rating: pilot rating scale for the piloted evaluation that complements the level verdicts. - flight-mechanics/stability-control/short-period-mode-analysis: source of the short period wn and zeta inputs to the model. ## Behavior contract (gate 3) Run the deterministic contract test (stdlib unittest, offline): python3 scripts/test_pitch_bandwidth_criteria.py The test covers the Case A and Case B worked examples against the spec reference numbers within tolerance, the lightly damped and low frequency trends, the gain margin branch (very low wn), the unwrapped phase helper and its consistency with the branch-corrected analytic phase, the bisection root finder on reachable and unreachable targets, magnitude versus transfer self consistency, the Level 1/2/3 verdict boundaries and missing metric reporting, and ValueError rejection of non-physical parameters and frequencies. ## Compliance - Standards referenced, not reproduced: MIL-STD-1797A section 4.5.1 frames the bandwidth and phase-delay criterion. The level boundaries coded in this leaf are representative Category A values and are class dependent in the standard, so verify them against the current revision before a certification-grade assessment. The transfer model and relations above are standard engineering methodology, summary-only per standards-map.yaml. - compliance: STANDARDS-REF, gated: false.