Accelerations due to the mass matrix parameters variation at 5.5 ms<sup>−</sup><sup>1</sup> of the airship speed.

Accelerations due to the mass matrix parameters variation at 5.5 ms<sup>−</sup><sup>1</sup> of the airship speed.

<p>Accelerations due to the mass matrix parameters variation at 5.5 ms<sup>−</sup><sup>1</sup> of the airship speed.</p>

محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Muhammad Wasim (8319120) (author)
مؤلفون آخرون: Ahsan Ali (6478244) (author), Faisal Saleem (1872289) (author), Inam Ul Hasan Shaikh (11654934) (author), Jamshed Iqbal (82302) (author)
منشور في: 2025
الموضوعات:
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
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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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