Configuration Dependent Stability Domain

Definition

The configuration-dependent stability domain is the subset of manipulator
configurations for which the closed-loop tracking error dynamics of a space
manipulator are asymptotically stable. Because the dynamic-coupling coefficients that enter
the error dynamics are functions of the joint angles (and of the base attitude), some
configurations satisfy the stability conditions and others do not; the admissible set therefore
has a configuration-dependent boundary, not a fixed one. In rutkovskii2023control
the domain is derived for a free-FLYING robot (fully-actuated, gas-jet base plus electromechanical
arm) installing a payload: it is the region in the joint-angle plane where the
end-point regulation loop stays stable, used to pick the initial configuration and bound the
admissible joint excursion during the operation. It generalizes the notion of a singularity-free
region (notation.md) from a purely kinematic rank condition to a dynamic, closed-loop
stability condition.

Key Equations

Symbols per notation.md. The joint angles , the
configuration-dependent coupling coefficients , and their determinant
are local to rutkovskii2023control and are not
in notation.md (do not confuse with any canonical symbol).

Linearized end-point error dynamics under PD control (12)–(13) yield the characteristic
polynomial , whose Routh-Hurwitz coefficients depend on the
coupling determinant

The configuration-dependent stability domain is then the joint-angle region satisfying the
sign condition (necessary for )

where is the base attitude and the fixed end-link angle. Where
the regulated coordinates become
unstable, so the domain boundary is set by the configuration-dependent sign of the coupling, not
by actuator limits.

Source Support

  • rutkovskii2023control — primary and sole source: derives
    the stability domain in joint-angle coordinates from a
    Routh-Hurwitz analysis of the linearized end-point error dynamics, and shows its topology depends
    on base attitude (more) and the gripper angle (less), Fig. 2. Free-FLYING
    regime (actuated base); contrasts explicitly with the paper’s free-FLOATING mode (attitude
    control disabled), where the working area narrows and dynamic singularities appear.
  • lyapunov_stability — the domain is the set where the closed-loop error
    has an asymptotically stable equilibrium; here certified via Routh-Hurwitz on the linearized
    characteristic polynomial rather than a Lyapunov function.
  • dynamic_coupling — the coefficients encode
    basearm coupling; their configuration dependence is precisely what makes the
    stable set configuration-dependent.
  • coordinated_control — the domain bounds where coordinated base-plus-arm
    regulation of the end point stays stable; it informs initial-configuration selection and admissible
    joint excursion.
  • ffsm_dynamics — the coupling coefficients descend from the FFSM equations of
    motion; the linearization (small joint rates) is what reduces them to the form.
  • technical_controllability — the source’s prior admissibility
    condition; the stability domain is a stronger, closed-loop requirement layered on top.

Open Questions

  • The domain is derived for a planar, linearized (small-rate), self-braking-actuator case; does
    the characterization survive in 3-D and at higher joint rates, where the neglected
    velocity-product terms re-enter?
  • The source bounds stability via a static sign condition on along a
    quasi-static install; how does this relate to the kinematic singularity-free region and
    to the dynamic thresholds used elsewhere in this wiki for the fully-coupled FFSM?