Aerospace Science and Technology
Designing the Nonlinear Guidance Law Adaptable to Initial Deviations for the Vertical Landing of the Booster

Morteza Sharafi; Nasser Rahbar; Ali Moharrampour; Abdorreza Kashaninia

Volume 15, Issue 1 , June 2022, , Pages 14-25

https://doi.org/10.22034/jast.2022.327899.1113

Abstract
  This study proposes a new non-linear guidance law for a Falcon 9 missile booster landing's terminal phase using a non-linear vectorized high expansion method. For this purpose, At first, the dynamic modeling of the landing problem is presented, assuming mass, gravity, and density are variables. Then, ...  Read More