Recent interests in Loss-of-Control (LOC) related accidents of aircraft bring back focus on the need for construction of realistic simulations not only of impending accident scenarios but also of recovery of aircraft from fully developed accident scenarios. Developing control schedules for both the activities thereby becomes crucial. In this paper, a novel approach based on constrained numerical continuation procedure is presented to effectively compute open-loop control interconnect schedules for a six-degree-of-freedom aircraft model. For illustrative purposes, the approach based on a new formulation of constraint equations is used to design open-loop control interconnect schedule for recovery of an F-18 HARV model from auto-rotational spin condition. Copyright © 2020 The Authors. This is an open access article under the CC BY-NC-ND license