Titlebook: Advances in Small Satellite Technologies; Proceedings of 1st I PSR Srinivasa Sastry,Jiji CV,Samba Siva Rao Conference proceedings 2020 Spri

Coarctation

書目名稱Advances in Small Satellite Technologies影響因子(影響力)




書目名稱Advances in Small Satellite Technologies影響因子(影響力)學(xué)科排名




書目名稱Advances in Small Satellite Technologies網(wǎng)絡(luò)公開度




書目名稱Advances in Small Satellite Technologies網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Advances in Small Satellite Technologies被引頻次




書目名稱Advances in Small Satellite Technologies被引頻次學(xué)科排名




書目名稱Advances in Small Satellite Technologies年度引用




書目名稱Advances in Small Satellite Technologies年度引用學(xué)科排名




書目名稱Advances in Small Satellite Technologies讀者反饋




書目名稱Advances in Small Satellite Technologies讀者反饋學(xué)科排名

falsehood

STANT

LAPSE

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

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

躲債

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.

虛情假意

Militia

LUT