The work is devoted to the synergetic synthesis of the harmonic disturbance asymptotic observerfor the aircraft hierarchical control system. The paper contains the general description of “flying platform”type vertical take-off & landing aircraft & an asymptotic observer of external disturbing influences(for example, wind) that have a harmonic dynamics & cause periodic changes in flight height, aswell as in pitch & roll angles. An asymptotic observer must ensure the asymptotic stability of a reservedsystem, the implementation of technological invariants, the estimation of unobservable external influencesfrom the current values of the observed state-space variables, & the absorption of harmonic winddisturbances. The article also presents an extended mathematical model of the “flying platform” in thevertical movement mode under external harmonic disturbing influences, including a mathematical descriptionof the disturbance dynamics, & the upper hierarchy level control algorithms based on thegiven technological invariants are synthesized. In addition, the equations of the disturbing influencesasymptotic observer are calculated, which supplement the mathematical model of the “flying platform”under disturbed motion, & the equations for asymptotic estimates of unobserved variables are calculated,which are further included in the upper hierarchy level control laws. The possibility of the disturbanceobserver synthesis was verified using the observability criterion. Finally, the results of computersimulation of the upper & the lower hierarchy levels’ nonlinear dynamics under disturbed motion withsuppression of external disturbances by an asymptotic observer are shown, as well as the results ofcomputer simulation of the vehicle’s nonlinear dynamics under disturbed motion without an asymptoticobserver to allow a visual assessment of the observer’s performance by comparison. The relevance ofthe work consists in the necessity of “flying platform” type vertical take-off & landing aircraft creationto increase the effectiveness of people rescue operations in those disaster areas where helicopters &other modern means don’t cope with a task. The scientific novelty of the work consists in synergeticapproach application to the design of the vehicle’s spatial position system equipped with an asymptoticobserver to suppress disturbing influences.
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