105 results on '"Lungu, Romulus"'
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2. Adaptive control of DGMSCMG using dynamic inversion and neural networks
3. Adaptive Control of the Relative Position for Space Vehicles in the Rendezvous Missions
4. Robust Optimal Control of Spacecraft during the Rendezvous Missions using H∞ Control Method
5. Software And Hardware Platform Using Dynamic Inversion And Neural Networks For The Launch Vehicles
6. Automatic Control of Launch Vehicles' Flight Path Slope Angle by Means of the Backstepping Control Method
7. Neural network based adaptive control of airplane’s lateral-directional motion during final approach phase of landing
8. Automatic landing system using neural networks and radio-technical subsystems
9. Application of H2/H∞ and dynamic inversion techniques to aircraft landing control
10. Aircraft Landing Control Using the H-inf Control and the Dynamic Inversion Technique
11. Reduced Order Observer for Linear Time-Invariant Multivariable Systems with Unknown Inputs
12. Dynamic Inversion based Control of DGMSCMGs. Part 2: Control Architecture Design and Validation
13. Dynamic Inversion based Control of DGMSCMGs. Part 1: Obtaining the Nonlinear Dynamic Model
14. Backstepping Control of Magnetically Suspended Double-Gimbal Control Moment Gyroscope
15. Backstepping and Dynamic Inversion based Autolanding System for Variable Centre of Mass UAV
16. Multiple Observer with Applications to Landing in Lateral-Directional Plane
17. Adaptive Neural Network-Based Satellite Attitude Control by Using the Dynamic Inversion Technique and a VSCMG Pyramidal Cluster
18. Reduced-order Multiple Observer with Application to the State Estimation of a Controlled Generic Reentry
19. Flight control of a launch vehicle using the hierarchical structured dynamic inversion with three time-scales
20. Automatic Control of Space Vehicles' Orbit around Earth
21. Sliding Mode Control of Launch Vehicles' Flight Path Slope Angle
22. Reduced-Order Multiple Observer Design for Takagi-Sugeno Models with Unknown Inputs
23. Autonomous Adaptive Control System for Airplane Landing
24. Aircraft Landing Control Using the H-inf Control and the Dynamic Inversion Technique
25. The control of airplane landing in longitudinal and lateral-directional planes by using the H-inf control
26. Complete landing autopilot having control laws based on neural networks and dynamic inversion
27. Automatic control of the microaerial vehicles’ attitude and position
28. The influence of atmospheric turbulences on aircraft landing process
29. Adaptive flight control for a launch vehicle based on the concept of dynamic inversion
30. Autonomous Adaptive Control System for Airplane Landing.
31. Landing Auto‐Pilots for Aircraft Motion in Longitudinal Plane using Adaptive Control Laws Based on Neural Networks and Dynamic Inversion
32. Adaptive flight control law based on neural networks and dynamic inversion for micro-aerial vehicles
33. Reduced-Order Multiple Observer for Aircraft State Estimation during Landing
34. Estimation of aircraft state during landing by means of multiple observers
35. Control of aircraft landing using the dynamic inversion and the H-inf control
36. Automatic control of the satellites' attitude and stored energy using inertial wheels
37. Automatic control of aircraft lateral-directional motion during landing using neural networks and radio-technical subsystems
38. Design of Automatic Landing Systems Using the H-inf Control and the Dynamic Inversion
39. Application of H 2 /H ∞ and dynamic inversion techniques to aircraft landing control
40. Four-Bar Mechanism's Proportional-Derivative and Neural Adaptive Control for the Thorax of the Micromechanical Flying Insects
41. Application Of H2/H∞Technique To Aircraft Landing Control
42. Automatic Control of Aircraft in Lateral-Directional Plane During Landing
43. Determination and Control of the Satellites’ Attitude by using a Pyramidal Configuration of Four Control Moment Gyros
44. Automatic control of the microaerial vehicles' attitude and position.
45. Landing Auto-Pilots for Aircraft Motion in Longitudinal Plane using Adaptive Control Laws Based on Neural Networks and Dynamic Inversion.
46. Adaptive Control of Helicopter Pitch Angle and Velocity
47. Design of Full‐Order Observers for Systems with Unknown Inputs by Using the Eigenstructure Assignment
48. Automatic landing control using H-inf control and dynamic inversion
49. ALSs with Conventional and Fuzzy Controllers Considering Wind Shear and Gyro Errors
50. Optimal control of MAVs' gliding motion - Part 2: Controller design and validation
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