Please use this identifier to cite or link to this item: http://idr.nitk.ac.in/jspui/handle/123456789/7191
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dc.contributor.authorBalakrishnan, B.
dc.contributor.authorShamrao
dc.contributor.authorAditya, R.
dc.contributor.authorNarendra, Nath, S.
dc.contributor.authorNarayana, S.
dc.contributor.authorPrasad, R.V.
dc.date.accessioned2020-03-30T09:58:37Z-
dc.date.available2020-03-30T09:58:37Z-
dc.date.issued2018
dc.identifier.citationInternational Conference on Ubiquitous and Future Networks, ICUFN, 2018, Vol.2018-July, , pp.53-58en_US
dc.identifier.urihttp://idr.nitk.ac.in/jspui/handle/123456789/7191-
dc.description.abstractDrones developed for interplanetary space missions require full autonomy of operations including safe landing and hovering due to the delay in communication. For operation in low atmospheric densities, coaxial helicopters are best suited and they are capable of handling manoeuvres due to their small footprints and ease of operation. However, the dynamics of the helicopter is coupled in lateral axes which need to be compensated for precise control. The present solutions include vision-based tracking in order to decouple the dynamics, which needs additional hardware. In this paper, a decoupling controller is presented that employs an accelerometer-based force feedback system for measuring the undesired forces in off-axis which does not need any additional hardware. The simulation results indicate that the force feedback methodology is very effective in controlling the off-axis drift of the coaxial helicopter. � 2018 IEEE.en_US
dc.titleActive Decoupling Control for a Planetary Coaxial Helicopter Using Force Feedbacken_US
dc.typeBook chapteren_US
Appears in Collections:2. Conference Papers

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