Pages that link to "Item:Q2576159"
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The following pages link to Spacecraft attitude control using explicit model predictive control (Q2576159):
Displaying 19 items.
- Theoretical and algorithmic advances in multi-parametric programming and control (Q373189) (← links)
- MPC on manifolds with an application to the control of spacecraft attitude on SO(3) (Q503190) (← links)
- Attitude estimation and control of manoeuvring spacecraft (Q1061700) (← links)
- Attitude tracking control for reentry vehicles using centralised robust model predictive control (Q2081837) (← links)
- Robust and fault-tolerant spacecraft attitude control based on an extended-observer design (Q2089114) (← links)
- Invariant extended Kalman filter on matrix Lie groups (Q2174001) (← links)
- Continuous-time model predictive control of under-actuated spacecraft with bounded control torques (Q2374479) (← links)
- Anti-unwinding sliding mode attitude control via two modified Rodrigues parameter sets for spacecraft (Q2665144) (← links)
- Event-driven model predictive control of timed hybrid Petri nets (Q2925108) (← links)
- Variable-structure control of spacecraft attitude maneuvers (Q3809677) (← links)
- Self-tuning control of attitude and momentum management for the Space Station (Q4006376) (← links)
- Attitude tracking control of a flexible spacecraft under angular velocity constraints (Q4967662) (← links)
- Model-free Adaptive Control for Spacecraft Attitude (Q5276871) (← links)
- Application of discrete time sliding mode control to a spacecraft in 6DoF with parameter identification (Q5391438) (← links)
- Field programmable gate array based predictive control system for spacecraft rendezvous in elliptical orbits (Q5745038) (← links)
- Stochastic model predictive control-based countermeasure methodology for satellites against indirect kinetic cyber-attacks (Q6134198) (← links)
- Design and validation of an MPC controller for CMG-based testbed (Q6159474) (← links)
- Sharper Bounds for Proximal Gradient Algorithms with Errors (Q6188503) (← links)
- Novel extended Kalman filter + H∞$$ {\mathbf{H}}_{\infty } $$ optimal output feedback control configuration for small satellites with high pointing stability requirements (Q6198184) (← links)
