Control system and method for erection of carrier rocket

Abstract

The invention provides a control system and method for erection of a carrier rocket. The control system comprises a control system body, a signal collecting system and an executing mechanism. The control system and method have the functions of automatic leveling, automatic weak leg detection and secondary leveling for a launching platform. By means of the control system and method, an erection device can be made to hold the rocket, full automatic erection is achieved, the rocket can safely and reliably land on the launching platform, and the total erection time is not longer than 10 min; a rocket holding mechanism on the erection device can be rapidly opened; a rocket supporting device and bearing device can automatically ascend and descend; and the erection device can quickly fall back before the rocket is about to be launched.

Description

technical field [0001] The invention relates to an erection control system of a carrier rocket. Background technique [0002] With the development of aerospace technology and the emergence of various new types of launch vehicles, a new type of launch method has emerged abroad, that is, the "three flat and one vertical" method. The main features of this launch scheme are: in the "three vertical and one distant" launch scheme, the fixed tower on the launch position is canceled and replaced by a movable erector. At the same time, it also plays the role of erecting the rocket as a whole and quickly falling back before shooting. At the same time, it needs the self-leveling of the launch platform and automatic detection of virtual legs, the release of the rocket's holding mechanism when it is vertically positioned, the support device and the receiving device. Automatic lift. This launch method can carry out simple, fast and automatic test and launch tasks in a site with simple f...

AI Technical Summary

Problems solved by technology

[0003] Based on the characteristics of the "three flats and one vertical" launch method of the launch vehicle under the new situation, after the erecting device transports the arrow to the launch position, it is necessary to erect the rocket as a whole through the erecting device and put the rocket on the launch pad stably At the same time, before the rocket is about to shoot, it is necessary to open the holding mechanism on the erecting device and quickly return the erecting device itself. At present, this technology has no application precedent in domestic launch vehicles, and there is no design experience for reference. Therefore, it is urgently needed Develop an engineering control software to realize the various functional requirements of the new rocket launcher and launch platform

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