Tianwen-1,the first mission of China’s planetary exploration program,accomplished its goals of orbiting,landing,and roving on the *** entry,descent,and landing(EDL)phase directly determines the success of the entire ...
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Tianwen-1,the first mission of China’s planetary exploration program,accomplished its goals of orbiting,landing,and roving on the *** entry,descent,and landing(EDL)phase directly determines the success of the entire mission,of which the guidance,navigation,and control(GNC)system is *** paper outlines the Tianwen-1 EDL GNC system design by introducing the GNC requirements followed by presenting the GNC system architecture and algorithms to meet such *** actual flight results for the whole EDL phase are also provided in this paper.
The visual recognition of sheet metal parts is a crucial component of industrial automation sorting, particularly under complex lighting and background interference conditions. To enhance the accuracy of sheet metal p...
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For the vehicle routing problem, this paper introduces a baseline function computation approach with “Detour Estimation” in deep reinforcement learning. During the training process, if a truck still has feasible cus...
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ISBN:
(数字)9798350387780
ISBN:
(纸本)9798350387797
For the vehicle routing problem, this paper introduces a baseline function computation approach with “Detour Estimation” in deep reinforcement learning. During the training process, if a truck still has feasible customers to serve every time it prepares to return to the depot, it is considered that the truck has taken a detour, and at this moment, the detour estimation for this partial solution is calculated, referred to as “partial detour estimation.” After completing the service of all customers and returning to the depot, the overall detour estimation of the entire delivery path is calculated based on a rule that gives less weight to earlier detour estimations, known as “overall detour estimation.” This paper computes the REINFORCE algorithm’s baseline by subtracting the “overall detour estimation” from the “true path length” to expedite algorithm’s convergence and enhance solution quality. Experimental results show that the method proposed in this paper, when applied to problems of size 20, 50, and 100, reduces the deviation from the optimal solution compared to the baseline calculation method in the original paper by 0.5 at most, respectively, demonstrating the effectiveness of the algorithm.
In adaptive grinding task, robotic arms are required to autonomously achieve uniform grinding of workpieces. This brings a great challenge to estimation and planning techniques. In this paper, a double-layer planning ...
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ISBN:
(数字)9798350380903
ISBN:
(纸本)9798350380910
In adaptive grinding task, robotic arms are required to autonomously achieve uniform grinding of workpieces. This brings a great challenge to estimation and planning techniques. In this paper, a double-layer planning framework is designed to make industrial robotic arms accomplish adaptive grinding tasks for various tee tubes of arbitrary size, spatial orientation and surface characteristic. Dynamic-hierarchical-ant-colony-system (DHACS) and velocity-vector-decomposition-based (VVD-based) parameterized path planning are designed and applied to calculate the optimal grinding order and generate grinding paths along tee tube surfaces. Experimental results demonstrate that the shortest grinding path along arbitrary tee tube is generated adaptively by the planning framework proposed. Compared to the state-of-the-art methods, the efficiency and effectiveness of the planning framework proposed in this paper are demonstrated. Specifically, in terms of optimal solution quality, the performance advantages are at least 1.224%, 4.629% and 3.673% respectively.
In order to evaluate the performance of wireless communication systems in a faster and more economic fashion, we propose to design the so-called channel simulator, through which wireless channel properties of complex ...
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In recent years, numerous technological advancements in Artificial Generative intelligences (AGIs) have demonstrated significant potential to transform the intelligence acquisition mechanisms in connected autonomous v...
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The event-triggered control with intermittent output can reduce the communication burden between the controller and plant side over the network. It has been exploited for adaptive output feedback control of uncertain ...
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In this study, we address the challenge of disturbance estimation in legged robots by introducing a novel continuous-time online feedback-based disturbance observer that leverages measurable variables. The distinct fe...
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Facing the increasingly crowded orbital space and the gradually increasing space threats, more attention needs to be paid to spacecraft safety in space. In order to address the problem of non-cooperative spacecraft...
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ISBN:
(纸本)9781450397056
Facing the increasingly crowded orbital space and the gradually increasing space threats, more attention needs to be paid to spacecraft safety in space. In order to address the problem of non-cooperative spacecraft's approach interference to our spacecraft, the process of non-cooperative spacecraft's approach to our spacecraft by using Hohmann transfer is given by Satellite Tool Kit (STK) software, and the whole process of spacecraft's abnormal orbital maneuvering to approach our spacecraft is identified and judged by the method based on long short-term memory (LSTM) network. The simulation verifies that the LSTM network achieves good results.
Novel combined model predictive control method is presented, which includes long-term trajectory planning, outer-loop model predictive trajectory and angular momentum control, and inner-loop attitude control. Firstly,...
Novel combined model predictive control method is presented, which includes long-term trajectory planning, outer-loop model predictive trajectory and angular momentum control, and inner-loop attitude control. Firstly, the influence of long-period perturbation characteristics on long term station keeping of geosynchronous satellite is fully considered, and the station keeping trajectory is optimized for 3 months to 6 months. Then, taking the long-term planning results as the reference trajectory and considering the engineering constraint model, the outer-loop control is realized within 7 days to 14 days, so that the position trajectory meets the planning expectations and meets the requirements of orbit and angular momentum optimal control. The inner loop control adopts the attitude control method considering the continuous torque effect of small thrust, so as to meet the requirements of real-time angular momentum and attitude control with higher frequency. The method has been successfully verified by on-orbit flight tests, showing the characteristics of high control accuracy, high fuel utilization efficiency, and being adaptive to various engineering constraints.
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