Coarctation
发表于 2025-3-21 16:40:47
书目名称Advances in Small Satellite Technologies影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0149704<br><br> <br><br>书目名称Advances in Small Satellite Technologies读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0149704<br><br> <br><br>
falsehood
发表于 2025-3-21 21:33:50
http://reply.papertrans.cn/15/1498/149704/149704_2.png
STANT
发表于 2025-3-22 00:33:01
http://reply.papertrans.cn/15/1498/149704/149704_3.png
LAPSE
发表于 2025-3-22 06:51:51
De-Tumbling Controller of NIUSAT: Design, Simulation and On-Orbit Performancet it takes reasonable measures to effectively reduce the tumbling of the satellite in a reasonable time. In this paper, we will describe the design details of the de-tumbling controller, digital simulation results and the on-orbit performance on board the NIUSAT nano-satellite.
ACE-inhibitor
发表于 2025-3-22 10:12:29
Optimal Nonlinear Dynamic Inversion-Based Flight Control System Design for an Aerospace Vehiclell as optimal dynamic inversion (ODI). Nonlinear dynamic inversion is the control synthesis technique in which the inherent dynamics of a dynamical system are cancelled out and replaced by desired performance parameters which are selected by the designer. Two-loop control structure is adopted based
Classify
发表于 2025-3-22 16:21:15
http://reply.papertrans.cn/15/1498/149704/149704_6.png
躲债
发表于 2025-3-22 17:12:20
Slew Rate and Control Constrained Spacecraft Attitude Maneuver with Reaction Wheel Failurey diagonal and (c) skew configuration with skew angle of 45°, are studied. The paper further discusses single reaction wheel failure conditions for all the three configurations and demonstrates satellite rest to rest maneuver within the slew rate and actuator limits.
虚情假意
发表于 2025-3-22 21:14:34
http://reply.papertrans.cn/15/1498/149704/149704_8.png
Militia
发表于 2025-3-23 02:16:17
http://reply.papertrans.cn/15/1498/149704/149704_9.png
LUT
发表于 2025-3-23 07:19:17
http://reply.papertrans.cn/15/1498/149704/149704_10.png