Study on Synthetic Evaluation of Human Performance in Manually Controlled Spacecraft Rendezvous and Docking Tasks
نویسندگان
چکیده
Abstact: Manually Controlled Spacecraft Rendezvous and Docking (MCRVD) is a complex and demanding task which requires astronauts to performe accurate control of the spacecraft in six-degree-of-freedom by hand. The purpose of this study is to measure the human performance in these tasks and to propose a mathematical model to evaluate MCRVD performance quantitatively.A ground simulated RVD platform was developed and 25 male volunteers aged 25-35 were selected. They performed a total number of 3500 experiments. According to the analysis of the control bias during MCRVD, it is found that these parameters are of stage characteristics. The process of MCRVD can be divided into three stages: tracking control stage (100m-20m distance), accurate control stage (20m-0m distance) and docking stage (0m). The performance indexes of tracking control stage and accurate control stage are relevant, while the precision index during docking reflects the difficulty of control in different degrees-of-freedom. Based on the characteristics of different parameters, several statistical techniques including the factor analysis, the entropy analysis, and expert scoring are utilized to analyze the weight coefficient of each performance index. After that we presented a novel multi-hiberarchy integrated evaluation method which includes four hiberarchy: the performance of the tracking control, the performance of the accurate control, the precision of docking and the result of docking. Finally,the method was utilized to analyze the human performance in MCRVD, which verifies the validity of our method.
منابع مشابه
Guidance and Control for Spacecraft Autonomous Rendezvous and Proximity Maneuvers using a Geometric Mechanics Framework
Autonomous rendezvous and proximity operations between a chaser spacecraft and a target space object, consist of autonomous controlled approach and controlled docking with or controlled capture of the target by the chaser. Guidance, navigation and control problems during autonomous rendezvous and proximity maneuvers between spacecraft are challenging, particularly when the target spacecraft or ...
متن کاملMethodology for Prototyping Increased Levels of Automation for Spacecraft Rendezvous Functions
The Crew Exploration Vehicle necessitates higher levels of automation than previous NASA vehicles, due to program requirements for automation, including Automated Rendezvous and Docking. Studies of spacecraft development often point to the locus of decisionmaking authority between humans and computers (i.e. automation) as a prime driver for cost, safety, and mission success. Therefore, a critic...
متن کاملSSC07-XIII-3 Autonomous Distributed LQR/APF Control Algorithm for Multiple Small Spacecraft during Simultaneous Close Proximity Operations
An autonomous distributed LQR/APF control algorithm for multiple small spacecraft during simultaneous close proximity operations has been developed. This research contributes to the control of multiple small spacecraft for emerging operation, which may include inspection, assembly, or servicing. A control algorithm is proposed which combines the control effort efficiency of the Linear Quadratic...
متن کاملCognitive Vision for Autonomous Satellite Rendezvous and Docking
We present a cognitively-controlled vision system that combines low-level object recognition and tracking with high-level symbolic reasoning for the purpose of solving difficult space robotics problems—satellite rendezvous and docking. The reasoning module, which encodes a model of the environment, performs deliberation to 1) guide the vision system in a taskdirected manner, 2) activate vision ...
متن کاملGuidance and Control for Spacecraft Autonomous Chasing and Close Proximity Maneuvers
Autonomous rendezvous and proximity operations between a chaser (or pursuer) spacecraft and a target space object consist of autonomous controlled approach and controlled docking with or controlled capture of the target by the chaser. Guidance, navigation and control problems during autonomous rendezvous and proximity maneuvers between spacecraft are challenging, particularly when the target sp...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
عنوان ژورنال:
دوره شماره
صفحات -
تاریخ انتشار 2011