Abstract
Practical interest for supplementing stability analysis by domain-of-att raction considerations in studying constant-control maneuvers is pointed out. Implications in cost of computing work of the free parameter choice are estimated. A technique is presented for defining the entire safe range of maneuver in terms of regions of allowable and actually attainable roll rate values and the corresponding aileron inputs. Gravity effects are considered to define peak-value corrections of limits on the steady-state values of system variables and to estimate the maximum allowable duration of a rolling maneuver. An illustration of how a Lyapunov function provides estimate of the domain of attraction is given.
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