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Keywords: attitude control
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Journal Articles
Article Type: Research-Article
J. Dyn. Sys., Meas., Control. September 2019, 141(9): 091006.
Paper No: DS-17-1636
Published Online: May 2, 2019
...Ruiyun Qi; Weiwei Su; Yizhen Meng For deep space probe subject to uncertain time-varying inertia matrix, unknown external disturbances, actuator faults, and misalignment, a fault-tolerant attitude controller is designed in this paper, which is based on adaptive control and fast terminal sliding...
Journal Articles
Article Type: Research-Article
J. Dyn. Sys., Meas., Control. January 2016, 138(1): 011006.
Paper No: DS-13-1327
Published Online: November 12, 2015
.... 27 08 2013 19 10 2015 spacecraft finite-time observer attitude control output feedback control input saturation. The development of effective spacecraft control system is demanded for advanced space missions to ensure rapid and accurate global response to different attitude...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. September 2011, 133(5): 051006.
Published Online: August 1, 2011
... aircraft control angular velocity control asymptotic stability attitude control closed loop systems compensation control system synthesis fault location space vehicles vehicle dynamics adaptive backstepping attitude stabilization additive actuator fault loss of actuator effectiveness...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. September 2011, 133(5): 051001.
Published Online: July 19, 2011
.... A numerical example is presented to show the numerical preferences of using Kane’s method in deriving the equations of motion and also the efficacy of the control scheme. Acquiring a zero magnitude for spacecraft attitude control moment approves the free-floating behavior of the space robot in which...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. January 2011, 133(1): 011009.
Published Online: December 22, 2010
... ( 1 ), pp. 1 – 9 . 10.1016/0094-5765(91)90002-M Singh , S. N. , 1987 , “ Robust Nonlinear Attitude Control of Flexible Spacecraft ,” IEEE Trans. Aerosp. Electron. Syst. 0018-9251 , AES-23 ( 3 ), pp. 380 – 387 . 10.1109/TAES.1987.310836 Oz , H. , and Mostafa , O...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. September 2010, 132(5): 051001.
Published Online: August 11, 2010
...Junyoung Park; Alan Palazzolo This paper presents the theory and numerical results of utilizing four gimbaled, magnetically suspended, variable speed flywheels for simultaneous satellite attitude control and power transfer (charge, storage, and delivery). Previous variable speed control moment gyro...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. July 2008, 130(4): 041005.
Published Online: June 5, 2008
...Junyoung Park; Alan Palazzolo; Raymond Beach Theory and simulation results have demonstrated that four, variable speed flywheels could potentially provide the energy storage and attitude control functions of existing batteries and control moment gyros on a satellite. Past modeling and control...
Journal Articles
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. January 2008, 130(1): 011006.
Published Online: December 18, 2007
... and sequential diagonal MIMO QFT designs. attitude control controllers design engineering position control robust control space vehicles MIMO systems robust control QFT position and attitude control spacecraft control flexible structures In the next two decades several ESA and NASA...
Journal Articles
Article Type: Technical Papers
J. Dyn. Sys., Meas., Control. September 2007, 129(5): 689–698.
Published Online: March 16, 2007
.... A nonlinear model is developed that describes the relative formation dynamics. This highly nonlinear position and attitude control problem is solved by employing a recently developed nonlinear control approach, called the θ - D technique. This method is based on an approximate solution to the Hamilton-Jacobi...
Journal Articles
Article Type: Technical Papers
J. Dyn. Sys., Meas., Control. December 2002, 124(4): 606–612.
Published Online: December 16, 2002
... weapons attitude control aerodynamics tracking feedback Maneuvering projectiles offer the potential for significant reduction in gun system ammunition use through improved hit probability. Increasing concerns over collateral damage, environmental damage, and efficiency of military operations...