首页>
外国专利>
LTD LIABILITY COMPANY amp; LDQUO COMPANY INVEST AND TECHNOLOGIES amp; RDQUO
LTD LIABILITY COMPANY amp; LDQUO COMPANY INVEST AND TECHNOLOGIES amp; RDQUO
展开▼
机译：有限责任公司和LDQUO公司投资与技术和RDQUO
展开▼
页面导航
摘要
著录项
相似文献
摘要
A method for pitch and yaw control includes forced rotation of aircraft (A) with respect to long axis, reception and transformation of modulated laser radiation to control signals and sending those to electric servo actuators. A speed of A required or effective aerodynamical control is maintained by means of main rocket engine, and stability and given accuracy of aiming is provided due to rebuilding of structure of control system at section of operation of main rocket engine by setting restriction of set angle of deviation of rudders and discrete change of parameters – transfer ratio of open-loop system, level of gravity force compensation signal and time response of filter.
展开▼
