odometer
发表于 2025-3-21 16:54:23
书目名称Compound Control Methodology for Flight Vehicles影响因子(影响力)<br> http://impactfactor.cn/if/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles影响因子(影响力)学科排名<br> http://impactfactor.cn/ifr/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles网络公开度<br> http://impactfactor.cn/at/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles网络公开度学科排名<br> http://impactfactor.cn/atr/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles被引频次<br> http://impactfactor.cn/tc/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles被引频次学科排名<br> http://impactfactor.cn/tcr/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles年度引用<br> http://impactfactor.cn/ii/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles年度引用学科排名<br> http://impactfactor.cn/iir/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles读者反馈<br> http://impactfactor.cn/5y/?ISSN=BK0231858<br><br> <br><br>书目名称Compound Control Methodology for Flight Vehicles读者反馈学科排名<br> http://impactfactor.cn/5yr/?ISSN=BK0231858<br><br> <br><br>
Oafishness
发表于 2025-3-21 21:19:45
Steel Concrete Composite Construction,sue for aerospace industry. In general, the spacecraft motion is governed by the so-called kinematic equations and dynamic equations . Actually, these mathematical descriptions are highly nonlinear and the conventional linear control techniques are not suitable for the control design.
引起
发表于 2025-3-22 01:59:44
http://reply.papertrans.cn/24/2319/231858/231858_3.png
承认
发表于 2025-3-22 08:20:35
http://reply.papertrans.cn/24/2319/231858/231858_4.png
Urologist
发表于 2025-3-22 12:34:03
Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation,sue for aerospace industry. In general, the spacecraft motion is governed by the so-called kinematic equations and dynamic equations . Actually, these mathematical descriptions are highly nonlinear and the conventional linear control techniques are not suitable for the control design.
Mystic
发表于 2025-3-22 12:59:38
Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances,he time derivatives of the orientation angles to the angular velocity vector and the dynamic equation which describes the time evolution of the angular velocity vector . In , passivity-based control is proposed to ensure the asymptotical convergence of the attitude tracking without angular velocity measurements.
Mystic
发表于 2025-3-22 19:28:13
http://reply.papertrans.cn/24/2319/231858/231858_7.png
横截,横断
发表于 2025-3-22 23:23:24
http://reply.papertrans.cn/24/2319/231858/231858_8.png
全面
发表于 2025-3-23 03:52:53
Fatigue of Steel Plated Structures, spacecraft . investigates the attitude tracking and disturbance rejection problems of spacecraft and converts attitude control into a global stabilization problem. In , some spacecraft-attitude tracking problems are resolved by HOSMC laws.
观察
发表于 2025-3-23 08:29:20
Steel Structures Design Based on Eurocode 3le for the task of intercepting a non-maneuvering target or a weakly maneuvering target. In practice, target acceleration can change rapidly. For intercepting a target with powerful maneuvering capability, the performance of PN is degraded and it may be ineffective for some orientations between missile and target.