Enhancing the kinematic quality of a single-axis stabilizing platform on a high-speed spinning-body aircraft
DOI:
https://doi.org/10.54939/1859-1043.j.mst.106.2025.10-17Keywords:
Stabilizing platform; Attitude determination; Spinning aircraft; Vibration absorber.Abstract
Within the orientation system, a single-axis stabilizing platform is employed to mitigate the effects of high-speed aircraft body rotation on the sensors. To analyze its kinematic characteristics, this paper develops a dynamic model of the stabilizing platform's motion. Misalignment between the platform's axis and the rotational axis of the spinning-body aircraft introduces disturbance components that affect stabilization quality. This paper proposes a solution to reduce platform oscillations by employing a viscous vibration absorber. Simulation results using MATLAB Simulink clearly demonstrate the effectiveness of this approach.
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