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91results about "Pressure difference control" patented technology

Propelling system mixing ratio control method considering parallel storage tank pressure difference

The invention discloses a propelling system mixing ratio control method considering parallel storage tank pressure difference. The method comprises the following steps of (1) setting a state parameterbefore controlling; (2) calculating the balance pressure of parallel oxidant tanks; (3) calculating the balance pressure of parallel combustion agent tanks; and (4) controlling the mixing ratio. According to the method, the actual on-orbit working condition that the pressure between the two parallel storage tanks is imbalance before the mixing ratio of a spacecraft parallel storage tank propelling system is controlled is considered, the calculation flow of the balance pressure between the two parallel storage tanks before mixing ratio control is given, the method is suitable for the state that the on-orbit pressure of the parallel storage tank propelling system is unbalanced, and the on-orbit efficient utilization of propellant is realized; and the main process and the sub-process are all-parametric, iterative loop, interpretation branch and other calculation modes are introduced, so that a calculation program is convenient to compile, and then the time for determining a control parameter is reduced.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY
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