A method of augmenting an airborne vehicle for short-period dynamics and stability by passive means is presented in this study.A trajectoryphase disturbance rejection capability is achieved for an unguided fin-stabili...A method of augmenting an airborne vehicle for short-period dynamics and stability by passive means is presented in this study.A trajectoryphase disturbance rejection capability is achieved for an unguided fin-stabilized vehicle by flexible mounting of the fins to the vehicle body.The deflecting fins lag the body oscillation such that the harmonic oscillation can be quickly dampened.The amount of fin deflection may be chosen by a hinge-line location;among other things,the vehicle damping behaviour is largely determined by this choice.Linear theory is applied and 6-DOF simulations are carried out to demonstrate the approach suitability for the task.展开更多
文摘A method of augmenting an airborne vehicle for short-period dynamics and stability by passive means is presented in this study.A trajectoryphase disturbance rejection capability is achieved for an unguided fin-stabilized vehicle by flexible mounting of the fins to the vehicle body.The deflecting fins lag the body oscillation such that the harmonic oscillation can be quickly dampened.The amount of fin deflection may be chosen by a hinge-line location;among other things,the vehicle damping behaviour is largely determined by this choice.Linear theory is applied and 6-DOF simulations are carried out to demonstrate the approach suitability for the task.
