Application of guidance laws to quadrotor landing Conference Paper uri icon

abstract

  • 2015 IEEE. Aerial vehicle landing is an open and challenging problem. This paper focuses on development of simple guidance laws for quadrotor landing with known GPS location - stationary and moving. The guidance laws are based on missile guidance principles, namely pure pursuit, line-of-sight, and pure proportional navigation. Comparison on the performance of these guidance laws is presented through Matlab simulations and ROS implementation.

name of conference

  • 2015 International Conference on Unmanned Aircraft Systems (ICUAS)

published proceedings

  • 2015 International Conference on Unmanned Aircraft Systems (ICUAS)

author list (cited authors)

  • Gautam, A., Sujit, P. B., & Saripalli, S.

citation count

  • 9

complete list of authors

  • Gautam, Alvika||Sujit, PB||Saripalli, Srikanth

publication date

  • June 2015

publisher