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Modifying a Scientific Flight Control System for Balloon... https://forum.drakon.su/viewtopic.php?f=207&t=6598 |
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Автор: | Владимир Паронджанов [ Понедельник, 17 Июнь, 2019 19:39 ] |
Заголовок сообщения: | Modifying a Scientific Flight Control System for Balloon... |
Marc Schwarzbach, Sven Wlach, Maximilian Laiacker. Modifying a Scientific Flight Control System for Balloon Launched UAV Missions // German Aerospace Center DLR // IEEE, 2015 Цитата: Figure 6: Drakon representation of launch detection code
4. SOFTWARE The autonomy of the autopilot software had to be increased, especially for possible phases of lost datalink with no possibility of manual intervention. These situations rarely occur in close range testing. Some of the logic implemented is dictated by the safety regulations of the flight test range. Another challenging phase is the release of the plane hanging from the balloon, where automation is most important since it is the point of maximum distance to the ground station and the process needs quick automatic sequencing. Mission execution For programming automatic mission state switching and safety logic our software had to be extended. Like the hardware of our system, the software is modular, so we could add components rather then having to alter existing code. To code these critical functions we are using the DRAKON Editor software originally developed for the Russian space program [8]. It allows to graphically program flow diagrams which are checked for consistency. C-code is generated from the diagrams. The start detection logic is shown in Fig. 6 as an example. |
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