Aeronautical and Space-Rocket Engineering
Control and testing of flying vehicles and their systems
Аuthors
*, **, ***Bauman Moscow State Technical University, MSTU, 5, bldg. 1, 2-nd Baumanskaya str., Moscow, 105005, Russia
*e-mail: aleksej_ne@mail.ru
**e-mail: trigonella@mail.ru
***e-mail: sergey.soloviev@scsc.ru
Abstract
The article considers the issue of a space vehicles status monitoring automated systems developing.
The goal of the work consists in analysis and application of the tools for flight control systems of conventional spacecraft improving.
The technique of a manned spacecraft current state status monitoring with account for affecting factors (an aircraft orbital movement parameters, structural specifics of an aircraft and ground-based control loop), as well as a throughput of radio communication circuit for telemetric information transmitting, sensor equipment capabilities, onboard measuring instrumentation and computing means were studied.
The conclusion was drawn, that the tasks of controlling processes automation while spacecraft flight control are not exhaustive.
Depending on the designation of an individual spacecraft or spacecraft orbital group not only the tasks and their aggregate set can change, but specific and independent assignments may arise as well.
With account for the current flight control practice in manned astronautics the approach at large to a space vehicles' on-board equipment status monitoring automated systems developing was formed. Automation of problems solving on telemetric information displaying and analysing coupled with information support of a specialist of the group of analysis allows increase the quality level of the managing group functioning. It is achieved through detecting an abnormal situation, potentially translating into emergencies, as well as operational provision of flight control operators with information over a wide range of the problems being solved.
The significance of the spacecraft status monitoring automated systems developing is being proved by the fact that it allows minimize the human factor in the process of a spacecraft control, increase information accessibility and ease-off the burden of analysis group specialist while performing routine operations.
The considered approach to the spacecraft status monitoring automated systems developing can be applied to both the process of of existing manned space vehicles flight control process improvement, and prospective manned spacecraft under development.
Keywords:
automated monitoring system, manned spacecraft, space vehicle, control, status monitoring, space vehicle, control, status analysis, flight, spacecraft flight control, emergency situation, telemetric informationReferences
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