Xianlu Wang

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Propellant sloshing, which induces perturbations to dynamic behavior of spacecraft, is a conspicuous problem. Thus, sloshing suppression during maneuver poses a challenge on spacecraft control design. Herein, the input shaping technique, which has been validated in reducing residual vibration of flexible structure, is applied on this subject. The input(More)
A differential game guidance law for an endoatmospheric interceptor missile steered by aero fins and reaction jets is developed in this paper with bounded controls. For a low-altitude endoatmospheric interceptor, the propellant of the reaction-jet control system (RCS) is restricted by the missile configuration. Considering propellant limits, the effect of(More)
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