Rate of change of accelerations due to the aerodynamic forces at 5.5 ms−1 speed of the airship.

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Bibliographic Details
Main Author:	Muhammad Wasim (8319120) (author)
Other Authors:	Ahsan Ali (6478244) (author), Faisal Saleem (1872289) (author), Inam Ul Hasan Shaikh (11654934) (author), Jamshed Iqbal (82302) (author)
Published:	2025
Subjects:	Inorganic Chemistry Computational Biology Space Science Environmental Sciences not elsewhere classified Biological Sciences not elsewhere classified Mathematical Sciences not elsewhere classified Chemical Sciences not elsewhere classified Information Systems not elsewhere classified unscented kalman filter uncertain nonlinear dynamics sliding mode controller simulation results show hovering payload deliveries fully autonomous perspective estimated lumped uncertainty robust adaptive control lumped model uncertainty many potential applications trajectory tracking control lumped model uncertainties wind disturbance estimation lyapunov stability analysis airship trajectory tracking model uncertainties wind disturbance ultimate control desired trajectory applications require xlink "> usmc ), robotic airship research studies proposed method paper addresses method solves major challenge investigated using important aspects comprehensive algorithm chattering problem bound constraint airship autonomy aerostatic platform
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Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.