Due to the consideration of safety,non-contact measurement methods are be-coming more acceptable.However,massive measurement will bring high labor-cost and low working efficiency.To address these limitations,this pape...Due to the consideration of safety,non-contact measurement methods are be-coming more acceptable.However,massive measurement will bring high labor-cost and low working efficiency.To address these limitations,this paper introduces a deep learning model for the antenna attitude parameter measurement,which can be divided into an an-tenna location phase and a calculation phase of the attitude parameter.In the first phase,a single shot multibox detector(SSD)is applied to automatically recognize and discover the antenna from pictures taken by drones.In the second phase,the located antennas’fea-ture lines are extracted and their attitude parameters are then calculated mathematically.Experiments show that the proposed algorithms outperform existing related works in effi-ciency and accuracy,and therefore can be effectively used in engineering applications.展开更多
Exact estimation of space object attitude parameters is a great challenge.The effectiveness of conventional attitude estimation approaches based on target sizes suffers a significant reduction when occlusion exists.Th...Exact estimation of space object attitude parameters is a great challenge.The effectiveness of conventional attitude estimation approaches based on target sizes suffers a significant reduction when occlusion exists.This paper proposes an innovative approach to estimate the attitude parameters for space objects based on inverse synthetic aperture radar(ISAR)image sequences.The formulation for nonlinear size constraints(NSC)is developed by accounting for the characteristics of object size variation in ISAR image sequences.The multi-start framework for global optimization and the Broyden-Fletcher-Goldfarb-Shanno(BFGS)based quasi-Newton iterative method are combined with and used for more accurate estimation of space object’s attitude parameters.Furthermore,the Cramer-Rao lower bound(CRLB)of attitude parameter estimates is derived.Comparative experiments demonstrate the effectiveness and robustness of the proposed method.展开更多
Space object observation requirements and the avoidance of specific attitudes produce pointing constraints that increase the complexity of the attitude maneuver path-planning problem.To deal with this issue,a feasible...Space object observation requirements and the avoidance of specific attitudes produce pointing constraints that increase the complexity of the attitude maneuver path-planning problem.To deal with this issue,a feasible attitude trajectory generation method is proposed that utilizes a multiresolution technique and local attitude node adjustment to obtain sufficient time and quaternion nodes to satisfy the pointing constraints.These nodes are further used to calculate the continuous attitude trajectory based on quaternion polynomial interpolation and the inverse dynamics method.Then,the characteristic parameters of these nodes are extracted to transform the path-planning problem into a parameter optimization problem aimed at minimizing energy consumption.This problem is solved by an improved hierarchical optimization algorithm,in which an adaptive parameter-tuning mechanism is introduced to improve the performance of the original algorithm.A numerical simulation is performed,and the results confirm the feasibility and effectiveness of the proposed method.展开更多
文摘Due to the consideration of safety,non-contact measurement methods are be-coming more acceptable.However,massive measurement will bring high labor-cost and low working efficiency.To address these limitations,this paper introduces a deep learning model for the antenna attitude parameter measurement,which can be divided into an an-tenna location phase and a calculation phase of the attitude parameter.In the first phase,a single shot multibox detector(SSD)is applied to automatically recognize and discover the antenna from pictures taken by drones.In the second phase,the located antennas’fea-ture lines are extracted and their attitude parameters are then calculated mathematically.Experiments show that the proposed algorithms outperform existing related works in effi-ciency and accuracy,and therefore can be effectively used in engineering applications.
文摘Exact estimation of space object attitude parameters is a great challenge.The effectiveness of conventional attitude estimation approaches based on target sizes suffers a significant reduction when occlusion exists.This paper proposes an innovative approach to estimate the attitude parameters for space objects based on inverse synthetic aperture radar(ISAR)image sequences.The formulation for nonlinear size constraints(NSC)is developed by accounting for the characteristics of object size variation in ISAR image sequences.The multi-start framework for global optimization and the Broyden-Fletcher-Goldfarb-Shanno(BFGS)based quasi-Newton iterative method are combined with and used for more accurate estimation of space object’s attitude parameters.Furthermore,the Cramer-Rao lower bound(CRLB)of attitude parameter estimates is derived.Comparative experiments demonstrate the effectiveness and robustness of the proposed method.
基金supported by the National Natural Science Foundation of China(No.11572019).
文摘Space object observation requirements and the avoidance of specific attitudes produce pointing constraints that increase the complexity of the attitude maneuver path-planning problem.To deal with this issue,a feasible attitude trajectory generation method is proposed that utilizes a multiresolution technique and local attitude node adjustment to obtain sufficient time and quaternion nodes to satisfy the pointing constraints.These nodes are further used to calculate the continuous attitude trajectory based on quaternion polynomial interpolation and the inverse dynamics method.Then,the characteristic parameters of these nodes are extracted to transform the path-planning problem into a parameter optimization problem aimed at minimizing energy consumption.This problem is solved by an improved hierarchical optimization algorithm,in which an adaptive parameter-tuning mechanism is introduced to improve the performance of the original algorithm.A numerical simulation is performed,and the results confirm the feasibility and effectiveness of the proposed method.
