2019
DOI: 10.1002/asjc.2246
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Robust finite‐horizon optimal control of autonomous helicopters in aggressive maneuvering

Abstract: There has been an increasing need for autonomous helicopters to have the ability to perform aggressive maneuvers. To achieve this, robust and high performance controllers are required to accurately drive the helicopters. In this paper, the robust compensator (RC) technique is applied to the classic finite‐horizon LQR approach to deal with the uncertainties, including nonlinearities, external disturbances, and other interference. The robust properties of the proposed method are analyzed, and it is proved that t… Show more

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Cited by 4 publications
(4 citation statements)
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References 27 publications
(25 reference statements)
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“…Then this lemma can be proved analogously as Theorem 1 of [49]. □ In this paper, a system satisfying ||x E (t)|| 2 2 ≤ 𝜖 is said to have 𝜖-robustness about the state trajectory.…”
Section: V(t) = −𝑓 Iv(t) − 𝑓 B δ(T) V(0) = 𝟎mentioning
confidence: 95%
See 2 more Smart Citations
“…Then this lemma can be proved analogously as Theorem 1 of [49]. □ In this paper, a system satisfying ||x E (t)|| 2 2 ≤ 𝜖 is said to have 𝜖-robustness about the state trajectory.…”
Section: V(t) = −𝑓 Iv(t) − 𝑓 B δ(T) V(0) = 𝟎mentioning
confidence: 95%
“…The scalar 𝑓 therein is a parameter [49]. Note that Equation ( 12) describes a filter who takes x(t) and u(t) as input in real time and continuously generates v(t) as output.…”
Section: 𝝈(T) = −𝑓 𝝈(T) + (A + 𝑓 I)x(t) + Bu(t)mentioning
confidence: 99%
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“…Due to the vertical take-off and landing (VTOL) capabilities in limited spaces, helicopters have been rapidly used in military and civil fields [1][2][3]. It is a challenging problem to design an effective control scheme for a helicopter in the presence of system uncertainties and external disturbances.…”
Section: Introductionmentioning
confidence: 99%