The accuracy of dynamic attitude propagation [PDF]
Propagating attitude by integrating Euler's equation for rigid body motion has long been suggested for the Earth Radiation Budget Satellite (ERBS) but until now has not been implemented. Because of limited Sun visibility, propagation is necessary for yaw
Chu, D., Harvie, E., Woodard, M.
core +1 more source
IET Control Theory & ApplicationsHerein, a control system and a fault tolerance method for the rotor positionable quadrotor are proposed. Quadrotors that have a variable structure are made for different purposes.
Matin Davoudi Dehkordi, Mohammad Danesh
doaj +1 more source
Tridyne attitude control thruster investigation Final report [PDF]
Experimental results of feasibility Tridyne attitude control ...
Barber, H. E., Buell, C. H.
core +1 more source
Report of the Attitude Control and Attitude Determination Panel [PDF]
Failures and deficiencies in flight programs are reviewed and suggestions are made for avoiding them. The technology development problem areas considered are control configured vehicle design, gyros, solid state star sensors, control instrumentation ...
core +1 more source
Usability evaluation of attitude control for a robotic wheelchair for tip mitigation in outdoor environments. [PDF]
Med Eng Phys, 2020 Sivakanthan S +9 more
europepmc +1 more source
Model-reference attitude control and reaction control jet engine placement for space shuttle [PDF]
Analytical studies on the theoretical aspects of thrust vector control of large space vehicles were conducted. A system for attitude control of the space shuttle vehicle was developed.
Boland, J. S., III
core +1 more source
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System. [PDF]
Sensors (Basel), 2020 Feng C, Wang Q, Liu C, Hu C, Liang X.
europepmc +1 more source
Two Axis Pointing System (TAPS) attitude acquisition, determination, and control [PDF]
The Two Axis Pointing System (TAPS) is a 2 axis gimbal system designed to provide fine pointing of Space Transportation System (STS) borne instruments. It features center-of-mass instrument mounting and will accommodate instruments of up to 1134 kg (2500
Azzolini, John D., Mcglew, David E.
core +1 more source
AE-C attitude determination and control prelaunch analysis and operations plan [PDF]
A description of attitude control support being supplied by the Mission and Data Operations Directorate is presented. Included are descriptions of the computer programs being used to support the missions for attitude determination, prediction, and ...
Headrick, R. D. +3 more
core +1 more source
Low cost attitude control system scanwheel development [PDF]
In order to satisfy a growing demand for low cost attitude control systems for small spacecraft, development of low cost scanning horizon sensor coupled to a low cost/low power consumption Reaction Wheel Assembly was initiated.
Bialke, William, Selby, Vaughn
core +1 more source