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A Robust H ∞ Controller for an UAV Flight Control System.

López J, Dormido R, Dormido S, Gómez JP - ScientificWorldJournal (2015)

Bottom Line: A robust inner-outer loop strategy is implemented.The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft.The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements.

View Article: PubMed Central - PubMed

Affiliation: Dynamic Systems Research Group, Universidad Politécnica de Madrid (ETSIA/EUITA), Plaza Cardenal Cisneros 3, 28040 Madrid, Spain.

ABSTRACT
The objective of this paper is the implementation and validation of a robust H ∞ controller for an UAV to track all types of manoeuvres in the presence of noisy environment. A robust inner-outer loop strategy is implemented. To design the H ∞ robust controller in the inner loop, H ∞ control methodology is used. The two controllers that conform the outer loop are designed using the H ∞ Loop Shaping technique. The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft. The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements.

No MeSH data available.


Smooth psi angle reference.
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Related In: Results  -  Collection


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fig16: Smooth psi angle reference.

Mentions: The reference is provided to the autopilot as a psi angle function and is built in a soft way using a combination of a step and a ramp. The reference is shown in the Figure 16.


A Robust H ∞ Controller for an UAV Flight Control System.

López J, Dormido R, Dormido S, Gómez JP - ScientificWorldJournal (2015)

Smooth psi angle reference.
© Copyright Policy - open-access
Related In: Results  -  Collection

Show All Figures
getmorefigures.php?uid=PMC4477258&req=5

fig16: Smooth psi angle reference.
Mentions: The reference is provided to the autopilot as a psi angle function and is built in a soft way using a combination of a step and a ramp. The reference is shown in the Figure 16.

Bottom Line: A robust inner-outer loop strategy is implemented.The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft.The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements.

View Article: PubMed Central - PubMed

Affiliation: Dynamic Systems Research Group, Universidad Politécnica de Madrid (ETSIA/EUITA), Plaza Cardenal Cisneros 3, 28040 Madrid, Spain.

ABSTRACT
The objective of this paper is the implementation and validation of a robust H ∞ controller for an UAV to track all types of manoeuvres in the presence of noisy environment. A robust inner-outer loop strategy is implemented. To design the H ∞ robust controller in the inner loop, H ∞ control methodology is used. The two controllers that conform the outer loop are designed using the H ∞ Loop Shaping technique. The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft. The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements.

No MeSH data available.