Dynamic Modeling and Analysis of a Whole-Wing Micro Air Vehicle

Kuo, Zeal-Sain; Soong, Chyi–Yeou; Chang, Yun-Sheng

doi:10.2514/6.2007-2238

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Dynamic Equations1

Figure 31 Framework For Dynamic Analysis and Control Develo1

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2011

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Cited by 5 publications

(2 citation statements)

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“…Following the previous flight dynamics analyses [10,11], the classical system of scalar dynamic equations of a rigid, constant mass airplane in proximity of a flat-Earth with symmetric layout in the body-axis reference can be depicted by…”

Section: Dynamic Equationsmentioning

confidence: 99%

Dynamics modeling and control of large transport aircraft in heavy cargo extraction

Feng

Shi

Wei

2011

J. Control Theory Appl.

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In this paper, a novel version of six-degree-of-freedom nonlinear model for transport aircraft motion in cargo extraction is developed and validated by the theoretical mechanics and flight mechanics. In this model constraint force and moment reflecting the flight dynamic effects of inner moving cargo are formulated. A methodology for a control law design in this phase is presented, which linearizes the aircraft dynamics making use of piecewise linearization and utilizes robust control technique for interval system to achieve specified handling qualities with robustness to uncertainties. The simulations demonstrate adequate effectiveness and excellent robustness of the proposed controller.

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Section: Dynamic Equationsmentioning

confidence: 99%

Dynamics modeling and control of large transport aircraft in heavy cargo extraction

Feng

Shi

Wei

2011

J. Control Theory Appl.

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“…The main difference is on the frequency of the oscillatory motions, which is higher for UAVs / MAVs than for the large aircraft [51]. The airspeed variations might move the phugoid mode to the right half plane, while the short period and Dutch roll modes locations are relatively unaffected [52].…”

Section: Figure 31 Framework For Dynamic Analysis and Control Develomentioning

confidence: 99%

Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle

Setiawan¹

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Autonomous Flight Test of a Novel Nonconventional Biplane Micro Air Vehicle

Jana¹,

Shivkumar

Shewale

et al. 2022

J. Aerosp. Eng.

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Dynamic Modeling and Analysis of a Whole-Wing Micro Air Vehicle

Cited by 5 publications

References 2 publications

Dynamics modeling and control of large transport aircraft in heavy cargo extraction

Dynamics modeling and control of large transport aircraft in heavy cargo extraction

Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle

Autonomous Flight Test of a Novel Nonconventional Biplane Micro Air Vehicle

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