This paper focuses on the dynamic stability of rolling missiles equipped with angle-of-attack
feedback three-loop autopilot considering parasitic effect induced by radar radome slope. By …

The dynamic stability of a radar homing rolling missile is extremely complex due to the
interaction of the parasitic radome aberration feedback loop and the cross-coupling between …

The dynamic stability of coning motion for a radar homing rolling missile is studied in this
paper, and the parasitic radome loop is considered and introduced into the guidance system …

In this paper, the controller design and stability analysis for the parameters time-varying
model of spinning missiles are investigated. A mathematical model for the spinning missile …

This paper investigates the problem of coning motion stability of spinning missiles equipped
with strapdown seekers. During model derivation, it is found that the scaling factor error …

A one degree of freedom flight motion table is used to simulate the rotational movement of
flying objects in hardware‐in‐the‐loop laboratories. This table uses a dual motor driving …

Trajectory tracking guidance is employed widely by low cost missiles for the characteristic of
easy to implement. However, for spinning missile, the guidance loop may result in dynamic …

In this paper, the dynamic stability analysis of a rolling airframe actuated by one pair ON-
OFF actuator using linear theory is presented via developing a new closed form solution …

A novel attitude control scheme is proposed for a rolling aerial vehicle (RAV) with large
uncertainties. Firstly, the RAV highly coupled nonlinear system is separated into attitude …

Rolling airframe manoeuvring is a type of manoeuvre in which the missile provides
continuous roll during flight. Cross-coupling between the angle of attack and sideslip in …