Spacecraft using - Globe Thesis

Keyword [Spacecraft using] Result: 1 - 20 \| Page: 1 of 2
1.	Study On Vibration Isolation Of Flexible Spacecraft Using Viscoelastic Materials
2.	Autonomous Control Of Miniature Spacecraft Using Nonlinear Model Predictive Control
3.	Attitude Maneuver Control Of Spacecraft Using Angular Momentum Exchange
4.	Study On Vibration Isolation Of Spacecraft Using Non-probabilistic Reliability Theory
5.	Identification Of Mass Characteristic Parameters And Control Of Spacecraft Using Robotic Arm
6.	Research On Attitude Control Methods For Spacecraft Using Single-gimbal Control Moment Gyros
7.	Optimal Orbit Transfer For Continuous Thrust Spacecraft Using Sequential Convex Programming
8.	Relative navigation between two spacecraft using X-ray pulsars
9.	Optimal reorientation of spacecraft using only control moment gyroscopes
10.	LQG/LTR optimal attitude control of small flexible spacecraft using free-free boundary conditions
11.	Feedback control and steering laws for spacecraft using Canfield joint attitude manipulators
12.	Using neuromorphic optical sensors for spacecraft absolute and relative navigation
13.	On attitude recovery of spacecraft using nonlinear control
14.	Exploration of the region near the sun-earth collinear libration points for the control of large formations
15.	Control of spacecraft with flexible structures using pulse-modulated thrusters
16.	Operationally responsive spacecraft using electric propulsion
17.	Attitude dynamics and control of a spacecraft using shifting mass distribution
18.	Electromagnetic Propulsion System for Spacecraft using Geomagnetic fields and Superconductors
19.	Design of a carbon fiber composite grid structure for the GLAST spacecraft using a novel manufacturing technique
20.	Reorientations of flexible spacecraft using momentum exchange devices
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