ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

A Finite-Time Partial IGC Approach for Formation Flying with Collision Avoidance

Oza, Harshal and Padhi, Radhakant (2017) A Finite-Time Partial IGC Approach for Formation Flying with Collision Avoidance. In: IEEE Annual India Conference (INDICON), DEC 16-18, 2016, Bangalore, INDIA.

[img] PDF
2016_Iee_Ann_Ind_Com.pdf - Published Version
Restricted to Registered users only

Download (429kB) | Request a copy
Official URL: http://dx.doi.org/ 10.1109/INDICON.2016.7838987


A finite-time stable non-linear partial integrated guidance and control algorithm is proposed for formation flying. A Lyapunov based proof for the outer loop of the integrated guidance and control philosophy is furnished to provide an a priori guarantee of a collision-free guidance trajectory. The guidance and control structure retains the advantages of the time scale separation between the translational and rotational dynamics explicitly while also preserving the integrated two loop structure. Numerical simulation is presented to show the suitability of the proposed algorithm that takes advantage of the latest results in the area of non-linear finite time control.

Item Type: Conference Proceedings
Series.: Annual IEEE India Conference
Publisher: IEEE, 345 E 47TH ST, NEW YORK, NY 10017 USA
Additional Information: IEEE Annual India Conference (INDICON), Bangalore, INDIA, DEC 16-18, 2016
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 10 Jun 2017 04:42
Last Modified: 31 Oct 2018 13:59
URI: http://eprints.iisc.ac.in/id/eprint/57212

Actions (login required)

View Item View Item