Adaptive Air Ejection Device for Catapulting Cargo of the “Guided Air Missile” Type

摘要

This article presents the results of the development and research of an adaptive air ejection device for catapulting cargo of the “guided air missile” type. The principal diagram of the device based on the use of hydraulic drive pushers and stemming from an approach to controlling the ejection process taking into account the need to ensure safe separation of the payload, is demonstrated. The components of the system’s dynamics model are considered using Russian software products of SimInTech and EULER, computer simulation and full-scale experiments, confirming the operational integrity and correctness of the control system algorithms, are carried out.