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Spatiotemporal Variation and Driving Analysis of Net Primary Productivity of Vegetation in Southern Part of Taihang Mountain, China
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作者 Taiyi Cai chenglong he +1 位作者 Ammara Gill Chao Ma 《Journal of Environmental & Earth Sciences》 2025年第1期611-624,共14页
The net primary productivity of vegetation(NPP)is an important index to evaluate the carbon sequestration capacity of vegetation and land use change.Using MOD17N3HGF NPP data,climate data and night-time light data fro... The net primary productivity of vegetation(NPP)is an important index to evaluate the carbon sequestration capacity of vegetation and land use change.Using MOD17N3HGF NPP data,climate data and night-time light data from 2000 to 2020,this study explored the relationship between NPP and urban expansion,land use and climate change in the Southern Part of Taihang Mountain through brightness gradient method,trend analysis,partial correlation analysis and contribution analysis.It aims to provide information support for urban and rural planning and ecological management in this region.Key findings include:Over the past 20 years,NPP in mountain areas has shown an overall fluctuating upward trend,with an“N”pattern related to altitude.The human activity area expanded by 9.9%,with expansion of highly active areas holding back NPP growth and moderately active areas contributing to it.The trend of climate change is gradually warming and wetting,and the correlation between precipitation and NPP is strong,while the correlation between temperature and NPP is weak.Compared with human activities(19.9%),precipitation was the main driver of NPP change,contributing significantly up to 79.5%.In the past 20 years,the ecological quality of the south Taihang Mountain region has improved significantly and actively responded to climate change,but human activities have led to spatial and temporal ecological differences. 展开更多
关键词 Climate Change MODIS NPP Man-Land Relationship Southern Part of Taihang Mountain
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Study on Forced Straight-Line Guidance for the Final Translation Phase of Spacecraft Rendezvous 被引量:1
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作者 Baichun Gong chenglong he Degang Zhang 《Computer Modeling in Engineering & Sciences》 SCIE EI 2020年第1期207-219,共13页
Aimed at the problem of final translation of space rendezvous for the applications such as docking,inspection and tracking,optimal straight-line guidance algorithm based on pulse/continuous low-thrust in the context o... Aimed at the problem of final translation of space rendezvous for the applications such as docking,inspection and tracking,optimal straight-line guidance algorithm based on pulse/continuous low-thrust in the context of Clohessy-Wiltshire dynamics is proposed.Two modes of guidance strategy:varying-speed and fixed-speed approaching scheme for V-bar and R-bar approach by using constant/finite low-thrust propulsion respectively are studied,and the corresponding fuel-optimal conditions are obtained.Numerical simulation is conducted to verify and test the proposed algorithms.The results show that there is generally no different between the fuel consumptions by using the two different approaching modes for V-bar case.However,the conclusion for Rbar case is different that the using of continuous low-thrust cost more fuel and transfer time. 展开更多
关键词 Space rendezvous final translation straight line guidance
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Cooperative Angles-Only Relative Navigation Algorithm for Multi-Spacecraft Formation in Close-Range
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作者 Sha Wang chenglong he +2 位作者 Baichun Gong Xin Ding Yanhua Yuan 《Computer Modeling in Engineering & Sciences》 SCIE EI 2023年第1期121-134,共14页
As to solve the collaborative relative navigation problem for near-circular orbiting small satellites in close-range under GNSS denied environment,a novel consensus constrained relative navigation algorithm based on t... As to solve the collaborative relative navigation problem for near-circular orbiting small satellites in close-range under GNSS denied environment,a novel consensus constrained relative navigation algorithm based on the lever arm effect of the sensor offset from the spacecraft center of mass is proposed.Firstly,the orbital propagation model for the relative motion of multi-spacecraft is established based on Hill-Clohessy-Wiltshire dynamics and the line-of-sight measurement under sensor offset condition is modeled in Local Vertical Local Horizontal frame.Secondly,the consensus constraint model for the relative orbit state is constructed by introducing the geometry constraint between the spacecraft,based on which the consensus unscented Kalman filter is designed.Thirdly,the observability analysis is done and the necessary conditions of the sensor offset to make the state observable are obtained.Lastly,digital simulations are conducted to verify the proposed algorithm,where the comparison to the unconstrained case is also done.The results show that the estimated error of the relative position converges very quickly,the location error is smaller than 10m under the condition of 10−3 rad level camera and 5m offset. 展开更多
关键词 Relative navigation spacecraft formation observability analysis angles-only measurement
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