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Criterions and Measures of Route Selection of Shallowly Embedded Long-Distance Oil and Gas Pipeline in Mountain Areas 被引量:1
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作者 WANG Chenghua MA Qingwen +2 位作者 KONG Jiming CHEN Zefu LI Xiuzhen 《Wuhan University Journal of Natural Sciences》 EI CAS 2006年第4期787-792,共6页
According to the engineering investigation of long-distance oil and gas pipelines, the criterions and measures of route selection are drawn as follows: the flat landform is the first choice in route alignment. The fo... According to the engineering investigation of long-distance oil and gas pipelines, the criterions and measures of route selection are drawn as follows: the flat landform is the first choice in route alignment. The foot of mountain is the first choice when the route passes by the valley. The route should pass by but the shady and deposited slope and not in sunny and erosive slope as possible as it can. The pipeline should be vertical to contour climbing and descending the mountain except steep slope. Tunnel can be used in crossing foothill. Perpendicularly traversing the river is better than beveling; the worst choice is to put the pipeline along the river. Bypass is the best choice in karsts area. The order of route selection should be pre-choosing, investigation, optimization and adjustment. 展开更多
关键词 shallowly embedded long-distance oil and gas pipeline criterions and measures of route selection avoiding geological hazards
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Powered-descent landing GNC system design and flight results for Tianwen-1 mission 被引量:6
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作者 Xiangyu Huang Chao Xu +6 位作者 Jinchang Hu Maodeng Li Minwen Guo Xiaolei Wang Yu Zhao Baocheng Hua Yunpeng Wang 《Astrodynamics》 EI CSCD 2022年第1期3-16,共14页
The powered-descent landing(PDL)phase of the Tianwen-1 mission began with composite backshell–parachute(CBP)separation and ended with landing-rover touchdown.The main tasks of this phase were to reduce the velocity o... The powered-descent landing(PDL)phase of the Tianwen-1 mission began with composite backshell–parachute(CBP)separation and ended with landing-rover touchdown.The main tasks of this phase were to reduce the velocity of the lander,perform the avoidance maneuver,and guarantee a soft touchdown.The PDL phase overcame many challenges:performing the divert maneuver to avoid collision with the CBP while simultaneously avoiding large-scale hazards;slowing the descent from approximately 95 to 0 m/s;performing the precise hazard-avoidance maneuver;and placing the lander gently and safely on the surface of Mars.The architecture and algorithms of the guidance,navigation,and control system for the PDL phase were designed;its execution resulted in Tianwen-1’s successful touchdown in the morning of 15 May 2021.Consequently,the Tianwen-1 mission achieved a historic autonomous landing with simultaneous hazard and CBP avoidance. 展开更多
关键词 Tianwen-1 powered-descent landing(PDL) guidance navigation and control(GNC) backshell avoidance hazard avoidance
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