The phrase "aircraft dynamic" is correct and usable in written English.
It can be used in contexts related to aviation, particularly when discussing the behavior or characteristics of aircraft in flight.
Example: "The aircraft dynamic during the test flight revealed several areas for improvement in stability and control."
Alternatives: "aircraft behavior" or "aircraft performance".
The feedback linearizing controller is designed considering a nominal model of the aircraft dynamic.
The first phase of flight tests was performed with the goal of exciting all the aircraft dynamic modes.
As an application, such an adaptive controller is used for actuator failure compensation of a twin otter aircraft longitudinal model, with design conditions verified and control structure and adaptive laws developed for a nonlinear aircraft dynamic model.
This paper describes an application of a new fault detection and isolation (FDI) technique based on set-valued observers (SVOs) to a linear parameter varying (LPV) longitudinal aircraft dynamic model.
We applied the results on a F-8 aircraft-dynamic to validate the proposed approaches.
The aircraft dynamics are approximately linearized on-line using a dynamic inversion controller based on differential geometry theory.
During the wing morphing phase, the aircraft's dynamic response will be governed by time-varying aerodynamic forces and moments.
Aircraft flight dynamic characteristics can be greatly changed by ice accretion, which has been considered a considerable threat to aircraft flight safety for a long time.
Based on an aircraft system dynamic coupling feature and different actuator failure patterns, adaptive detectors are constructed to detect damage and actuator failures.
This numerical method evaluates the results from the conceptual approach, increases the numerical accuracy of the initial concept and the results are used for the Aircraft's Dynamic Stability analysis.
Special attention is paid to the following areas: ways to obtain the aerodynamic data of iced aircraft, flight dynamic modeling and simulation for iced aircraft, effects of ice accretion on aircraft stability and control as well as on flight performance and aircraft icing envelope protection and control adaption.
