DocumentCode
622653
Title
Planner test and analyzing system for deep space mission
Author
Fanyu Zhao ; Pingyuan Cui ; Rui Xu ; Ting Peng ; Dexiang Chen
Author_Institution
Beijing Inst. of Technol., Beijing, China
fYear
2013
fDate
12-14 June 2013
Firstpage
1224
Lastpage
1229
Abstract
As deep space exploration develops, onboard autonomy capability of the explorer becomes increasingly important, which requires the onboard planner to be more efficient. To improve the autonomy, a ground-based real-time fidelity simulation environment is needed, which enables rapid integration, testing and analyzing of the explorer planner. This paper describes the development of a Planner Test and Analysis System (PTAS) based on exploration mission. The planner modules under development include flight software, dynamic models, data interfaces, and monitoring module. Unified interface has been designed for application of planners with system level integration. The flight software includes attitude control subsystem, autonomous navigation, trajectory computing subsystem, and execution control subsystem. Planning result is analyzed by the flight software into executable commands on the embedded computer, and then transmitted to dynamic models on the multi-CPU computer, which makes PTAS a hardware-in-loop system. With some interfaces users could configure their own dynamic models. Simulation status about the explorer states and the process of mission simulation could be monitored, while planning and execution results could be analyzed quantitatively through a graphical interface, to show the planning efficiency and help users to improve the planner.
Keywords
aerospace computing; attitude control; control engineering computing; digital simulation; graphical user interfaces; mobile robots; multiprocessing systems; path planning; vehicle dynamics; PTAS; analyzing system; attitude control subsystem; autonomous navigation; data interfaces; deep space exploration; deep space mission; dynamic models; execution control subsystem; explorer planner analysis; explorer planner testing; flight software; graphical interface; ground-based real-time fidelity simulation environment; hardware-in-loop system; monitoring module; multiCPU computer; onboard autonomy capability; planner test-and-analysis system; trajectory computing subsystem; Attitude control; Computational modeling; Payloads; Planning; Software; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation (ICCA), 2013 10th IEEE International Conference on
Conference_Location
Hangzhou
ISSN
1948-3449
Print_ISBN
978-1-4673-4707-5
Type
conf
DOI
10.1109/ICCA.2013.6565124
Filename
6565124
Link To Document