Journal Articles

  1. Y. Qi, A. de Ruiter, “Transfers to Lunar Libration Point Orbits”, accepted for publication in Communications in Nonlinear Science and Numerical Simulation
  2. R. Gangapersaud, G. Liu, A. de Ruiter, “Detumbling a Non-cooperative Space Target with Model Uncertainties Using a Space Manipulator”, accepted for publication in Journal of Guidance, Control and Dynamics
  3. Y. Qi, A. de Ruiter, “Powered Swing-by in the Elliptic Restricted Three-body Problem”, accepted for publication in Monthly Notices of the Royal Astronomical Society
  4. Y. Qi, A. de Ruiter, “Low-energy Transfers to Long-term Capture in the Earth-Moon System” accepted for publication in Acta Astronautica
  5. D. Bolatti, A. de Ruiter, “Galerkin Variational Integrators for Orbit Propagation with Applications to Small-Bodies,” accepted for publication in Journal of Guidance, Control and Dynamics
  6. H. Gui, A.H.J de Ruiter, “Robustness Analysis and Performance Tuning for the Quaternion PD+ Attitude Controller”, accepted for publication in Journal of Guidance, Control and Dynamics
  7. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Comments on “Adaptive tracking control of uncertain MIMO nonlinear systems with input constraints” “, accepted for publication in Automatica
  8. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Disturbance observer-based attitude control for spacecraft with input MRS”, accepted for publication in IEEE Transactions on Aerospace and Electronic Systems
  9. Y. Qi, A. de Ruiter, “Study of Correction Maneuver for Lunar Flyby Transfers in the Real Ephemeris” accepted for publication in Journal of Guidance, Control and Dynamics
  10. Y. Qi, A. de Ruiter, “Energy Analysis in the Elliptic Restricted Three-body Problem”, accepted for publication in Monthly Notices of the Royal Astronomical Society
  11. Y. Qi, A. de Ruiter, “Short-term capture of the Earth-Moon system”, Monthly Notices of the Royal Astronomical Society, in press
  12. D. Ran, X. Chen, A. de Ruiter, “Adaptive extended state observer based fault tolerant attitude control for spacecraft with reaction wheels'”, accepted for publication in Acta Astronautica
  13. A. Frias, A.H.J. de Ruiter, K.D. Kumar, “Velocity-Free Attitude Stabilization of a Nadir-Pointing Underactuated Rigid Spacecraft”, accepted for publication in Journal of Guidance, Control and Dynamics
  14. H. Gui, A.H.J de Ruiter, “Global Finite-Time Attitude Consensus of Leader-Following Spacecraft Systems Based on Distributed Observers”, accepted for publication in Automatica
  15. A.H.J. de Ruiter, J.R. Forbes, M. Demjanenko, “Constrained Kalman Filtering,” accepted for publication in Journal of Guidance, Control and Dynamics
  16. H. Gui, A.H.J de Ruiter, “Adaptive Fault-Tolerant Spacecraft Pose Tracking with Control Allocation”, accepted for publication in IEEE Transactions on Control Systems Technology
  17. H. Gui, A.H.J de Ruiter, “Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation”, accepted for publication in Journal of Guidance, Control and Dynamics
  18. R. Hewitt, A. Ellery, A. de Ruiter, “Training a Terrain Traversability Classifier for a Planetary Rover Through Simulation,” accepted for publication in International Journal of Advanced Robotic Systems
  19. A. Zou, K.D. Kumar, A.H.J. de Ruiter, “Spacecraft Attitude Control Using Two Control Torques”, Information Sciences, Vol. 408,  2017, pp. 23-40
  20. H. Gui, A.H.J de Ruiter, “Control of Asteroid-Hovering Spacecraft with Disturbance Rejection Using Position-Only Measurements”, Journal of Guidance, Control and Dynamics, Vol. 40, No. 10 (2017), pp. 2401-2416
  21. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Finite-Time Attitude Tracking Control for Rigid Spacecraft with Control Input Constraints”, IET Control Theory and Applications, Vol. 11, No. 7, 2017, pp. 931-940
  22. A.H.J. de Ruiter and J.R. Forbes, “Continuous-Time O(n)-Constrained Kalman Filtering,” International Journal of Robust and Nonlinear Control, in press
  23. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Finite-Time Output Feedback Attitude Control for Rigid Spacecraft Under Control Input Saturation”, The Journal of the Franklin Institute, Vol. 353, No. 17, 2016, pp. 4442-4470 (pdf)
  24. A.H.J. de Ruiter and J.R. Forbes, “Discrete-Time SO(n)-Constrained Kalman Filtering,” AIAA Journal of Guidance, Control and Dynamics, Vol. 40, No. 1 (2017), pp. 28-37. (pdf)
  25. A.C. Vigneron, A.H.J. de Ruiter, B.V. Burlton, W.K.H. Soh, “Nonlinear Filtering for Autonomous Navigation of Spacecraft in Highly Elliptical Orbit,” Acta Astronautica,Vol. 126, 2016, pp. 138-149. (pdf)
  26. A.H.J. de Ruiter, L. Tran, B.S. Kumar, A. Muntyanov, “Sun Vector Based Attitude Determination of Passively Magnetically Stabilized Spacecraft,” AIAA Journal of Guidance, Control and Dynamics, Vol. 39, No. 7, 2016, pp. 1551-1562. (pdf)
  27. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Distributed attitude synchronization control for a group of flexible spacecraft using only attitude measurements”, Information Sciences, Vol. 343-344, 2016, pp. 66-78. (pdf)
  28. A.H.J. de Ruiter, “Quadratically Constrained Least Squares with Aerospace Applications”, AIAA Journal of Guidance, Control and Dynamics, Vol. 39, No. 3, 2016, pp. 487-497 (pdf)
  29. A. Zou, A.H.J. de Ruiter, K.D. Kumar, “Distributed Finite-Time Velocity Free Attitude Coordination Control for Spacecraft Formations”, Automatica, 67, 2016, pp. 46-53. (pdf)
  30. E.L. de Angelis, F. Giulietti, A.H.J. de Ruiter, G. Avanzini, “Spacecraft Attitude Control Using Magnetic and Mechanical Actuation”, AIAA Journal of Guidance, Control and Dynamics, Vol. 39, No. 3, 2016, pp. 564-573 (pdf)
  31. A.H.J. de Ruiter, “Observer-Based Adaptive Spacecraft Attitude Control with Guaranteed Performance Bounds”, IEEE Transactions on Automatic Control, 61 (10), 2016, pp. 3146-3151. (pdf)
  32. A. Zou, K.D. Kumar, A.H.J. de Ruiter, “Robust Attitude Tracking Control of Spacecraft Under Control Input Magnitude and Rate Saturations”, International Journal of Robust and Nonlinear Control, Vol. 26, No. 4, 2016, pp. 799-815. (pdf)
  33. A.H.J. de Ruiter, J.R. Forbes, “Generalized Euler Sequences Revisited”, Journal of the Astronautical Sciences, Vol. 62, No. 1, 2015, pp. 1-20. (pdf)
  34. S. Owlia, A. de Ruiter, “Autonomous Obstacle Avoidance for Fixed-Wing Unmanned Aerial Vehicles”, The Aeronautical Journal, Vol. 119, No. 1221, November 2015, pp. 1415-1436. (pdf)
  35. A. de Ruiter, “Computationally Simple Sub-Optimal Filtering for Spacecraft Motion Estimation”, Automatica, 57, 2015, pp. 105-112. (pdf)
  36. J. Forbes, A. de Ruiter, “Linear-Matrix-Inequality-Based Solution to Wahba’s Problem”, Journal of Guidance, Control and Dynamics, 38 (1), 2015, pp. 147-151. (pdf)
  37. A. de Ruiter, J. Forbes, “On the Solution of Wahba’s Problem on SO(n)”, Journal of the Astronautical Sciences, 60 (1), 2015, pp. 1-31. (pdf)
  38. J. Forbes, A. de Ruiter, D. Zlotnik, “Continuous-Time Norm-Constrained Kalman Filtering”, Automatica, 50 (10), 2014, pp. 2546-2554. (pdf)
  39. A. de Ruiter, J. Forbes, “General Identities for Parameterizations of SO(3) with Applications”, ASME Journal of Applied Mechanics, 81 (7), 2014. (pdf)
  40. A. de Ruiter “Some Applications of Passivity-Based Control and Invariance Principles”, IET Control Theory and Applications, 7 (7), 2013, pp. 1039-1048. (pdf)
  41. E.J. Findlay, A. de Ruiter, J.R. Forbes, H.H.T. Liu, C.J. Damaren, J. Lee, “Magnetic Attitude Control of a Flexible Satellite”, AIAA Journal of Guidance, Control and Dynamics, 36 (5), 2013, pp. 1522-1526. (pdf)
  42. A. de Ruiter, “Spacecraft Attitude Tracking with Guaranteed Performance Bounds”, AIAA Journal of Guidance, Control and Dynamics, 36 (4), 2013, pp. 1214-1221. (pdf)
  43. A. de Ruiter, “Improving Transient Performance in Computationally Simple Gyro-Corrected Satellite Attitude Determination”, Proc. IMechE, Part G: J. Aerospace Engineering, 226 (11), November 2012, pp. 1432-1444. (pdf)
  44. A. de Ruiter, “Magnetic Control of Dual-Spin and Bias Momentum Spacecraft”, AIAA Journal of Guidance, Control and Dynamics, 35 (4), July 2012, pp. 1158-1168. (pdf)
  45. A. de Ruiter, “A Fault-Tolerant Magnetic Spin Stabilizing Controller for the JC2Sat-FF Mission”, Acta Astronautica, 68 (1-2), January 2011, pp. 160-171. (pdf)
  46. B.S. Kumar, A. Ng, K. Yoshihara, A. de Ruiter, “Differential Drag as a Means of Spacecraft Formation Control”, IEEE Transactions on Aerospace and Electronic Systems, 47 (2), 2011, pp. 1125-1135. (pdf)
  47. A. de Ruiter, “Adaptive Spacecraft Attitude Tracking Control with Actuator Saturation”, AIAA Journal of Guidance, Control and Dynamics, 33 (5), 2010, pp. 1692-1696. (pdf)
  48. A. de Ruiter, “Adaptive spacecraft formation flying with actuator saturation”, Proc. IMechE, Part I: J. Systems and Control Engineering, 224 (4), 2010, pp. 373-385. (pdf)
  49. A. de Ruiter, “A Simple Suboptimal Kalman Filter Implementation for a Gyro-Corrected Satellite Attitude Determination System”, Proc. IMechE, Part G: J. Aerospace Engineering, 224 (7), 2010, pp. 787-802. (pdf)
  50. A.H.J. de Ruiter and H.H.T. Liu, “A Parameter Optimization Approach to Multiple-Objective Controller Design,” IEEE Transactions on Control Systems Technology, No. 2, Vol. 12, 2008, pp. 330–339. (pdf)
  51. Y. Kim, A.H.J. de Ruiter, J. Lee and A. Ng, “Robust Implementation of Kalman Filter for INS Correction,” Actual Problems of Aviation and Aerospace Systems: Processes, Models, Experiment, No. 3(25), Vol. 12, Kazan-Daytona Beach, 2007, pp. 55–74. (pdf)
  52. A.H.J. de Ruiter and C. Damaren, “Extended Kalman Filtering and Nonlinear Predictive Filtering for Spacecraft Attitude Determination,” Canadian Aeronautics and Space Journal, Vol. 48, 2002, pp. 13–24. (pdf)