Capture condition for endo-atmospheric interceptors steered by ALCS and ARCS

摘要: This contribution deals with capture condition for interceptor missiles steered by aero-lift control system (ALCS) and attitude reaction-jet (ARCS). With the guidance law derived from bounded differential game formulation, existence of zone is studied case that has advantage on maneuverability disadvantage agility. For open zone, ARCS can only close after engagement terminates. Moreover, also needs to contribute over minimum required value. More fuel will be if increases its maneuverability. The occurs at tangent point two curves: curve critical parameters a candidate constraint curve, which true even complex propellant constrain. validity these results demonstrated simulations.