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Nominal Stability Report

Preliminary FDM result: inertia, control derivatives, rate damping, and propulsion are placeholders; ADB v1.1 contains alpha-beta data only.

Database Metadata

  • File: adb_v1_1_drag_correction.csv
  • Moment/reference/CG: (-0.150, 0.000, 0.150) m
  • rho: 1.090 kg/m^3, q_ref: 340.625 Pa, S: 1.805 m^2, b: 3.950 m, c: 0.457 m

Trim

  • success: True
  • alpha: 1.5005 deg
  • theta: 1.5005 deg
  • elevator: 1.5157 deg
  • throttle: 0.1563
  • residual norm: 1.279e-13

Static Stability Derivatives

  • Cm_alpha: +0.985487 /rad (unstable longitudinal static sign)
  • Cn_beta: +0.024349 /rad (stable directional static sign)
  • Cl_beta: -0.010028 /rad (stable lateral static sign)
  • CL_alpha: +4.858682 /rad
  • CY_beta: -0.229180 /rad

Dynamic Modes

ModeEigenvalueswn rad/szetatime constant sClassification
phugoid-0.091489+0.764909j; -0.091489-0.764909j0.77040.118810.9303stable
short_period-11.7041+0j; +3.06093+0j3.0609-1.00000.3267unstable
dutch-roll-like lateral-directionalNo clearly identifiable Dutch-roll-like lateral-directional oscillatory mode was found in this linearization.n/an/an/anot identified
roll-30.229+0j30.22901.00000.0331stable
spiral-0.00898588+0j0.00901.0000111.2858stable

Summary

  • Static stability: longitudinal unstable, directional stable, lateral stable.
  • Dynamic stability among identified reduced-order modes: unstable.
  • Weakly damped modes: phugoid.
  • Unstable modes: short_period.
  • No clearly identifiable Dutch-roll-like lateral-directional oscillatory mode was found in this linearization. Because the aircraft uses an inverse V-tail/ruddervator layout and the current lateral reduced eigenspectrum is entirely real, treat this as a model limitation and classification ambiguity to investigate before flight-test use.

Conclusion

The nominal database is not an acceptable fixed-wing stability baseline in the current FDM workflow. It is statically unstable in pitch and has an unstable longitudinal dynamic mode, although it remains useful as the aft/reference starting point for the CG sensitivity sweep.