Adaptive second order sliding mode controller for vertical take-off and landing aircraft system

Mondal, Sanjoy; Gokul, T. V.; Mahanta, Chitralekha

doi:10.1109/iciinfs.2012.6304793

Cited by 2 publications

(2 citation statements)

References 21 publications

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“…The case of unmatched bounded disturbances is more involved. Nevertheless, under some posed conditions, it can be dealt with by suitably designed sliding mode control strategies [54]- [56].…”

Section: Sliding Mode Controllersmentioning

confidence: 99%

“Flyable” Guidance and Control Algorithms for Orbital Rendezvous Maneuver

Capello

Dabbene

Guglieri

et al. 2018

SICE Journal of Control, Measurement, and System Integration

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: Rendezvous orbital maneuvers are planned operations which intend to make two spacecraft meet, while avoiding collisions. Aspects such as trajectory safety and robustness, as well as obstacle avoidance, are fundamental for the mission success. The aim of this paper is to provide an overview of some recent algorithms for guidance and control systems, and also their combined exploitation, which can provide significant enhancements. This overview focuses on those algorithms that are characterized by key selected features: the discussed schemes guarantee low computational effort, low fuel consumption, and high safety and robustness. Different experimental setups, which can be used to evaluate the performance of the considered algorithms, are also taken into account and presented.

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Section: Sliding Mode Controllersmentioning

confidence: 99%

“Flyable” Guidance and Control Algorithms for Orbital Rendezvous Maneuver

Capello

Dabbene

Guglieri

et al. 2018

SICE Journal of Control, Measurement, and System Integration

View full text Add to dashboard Cite

show abstract

“…Reference [7] presented a second order sliding mode traction controller for road vehicles during skid braking and spin acceleration. Reference [8] proposed HOSMC for a highly complex nonlinear system suffering from the mismatched type of uncertainty caused by varying aerodynamic parameters and environmental disturbance in vertical take-off and landing aircraft system. References [9][10] designed a first-order sliding mode observers in the friction state.…”

Section: Introductionmentioning

confidence: 99%