Inverse optimal adaptive control for attitude tracking of spacecraft

By Wencheng Luo, Y. Chu, K. Ling. IEEE Transactions on Automatic Control, 2005

412 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/a6aafd460b3618ce7e5c2309500f575208760e09

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Yuanqing Xia
2. Shihua Li
3. Chunjiang Qian
4. Haibo Du
5. Zhenglong Zhu
6. M. Fu
7. Jie Huang
8. Ding Wang

In Control and Systems Engineering

1. Mou Chen
2. Shuzhi Sam Ge
3. Shaocheng Tong
4. Shihua Li
5. Beibei Ren
6. Haibo Du
7. Jie Huang
8. Yuanqing Xia

Citations in the corpus

• Attitude Tracking of Rigid Spacecraft With Bounded Disturbances (2011, methodology): “In [10], the inverse optimal adaptive control law combining the adaptive control approach and the optimal control method is designed to solve the attitude tracking problem of a rigid spacecraft.”
• Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control (2009, methodology): “As in [17], we suppose the desired attitude motion is generated by”
• Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization (2011, methodology): “Then, the relative kinematic equation is given as in [4] and the relative dynamic equation is given as in [5], [8]”
• Adaptive attitude tracking control for rigid spacecraft with finite-time convergence (2013, positive): “Spacecraft attitude dynamics and kinematics The attitude kinematics and dynamics of a rigid spacecraft can be modeled as (see Luo et al. (2005)): q̇v = 1 2 (q4I3 + q×v )Ω q̇4 = − 1 2 qTvΩ (2) JΩ̇ = −Ω×JΩ + u + d (3) here, the unit quaternion (qv, q4) ∈ R3 × R represents the attitude orientation of…”
• Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation (2011, background): “1: In spacecraft model equations (1) and (2), the unit-quaternion q and the angular velocity Ω are available in the feedback control design [2], [11].”
• Adaptive tracking control of uncertain MIMO nonlinear systems with input constraints (2011, positive): “In Luo et al. (2005), inverse optimal adaptive control was presented for the attitude tracking of spacecraft.”
• Model-Free Optimal Tracking Control via Critic-Only Q-Learning (2016, background): “For many practical systems, such as hypersonic aircraft [35]–[37], spacecraft [38], [39], motion tracking [40], etc.”
• Attitude stabilization of rigid spacecraft with finite‐time convergence (2011, methodology): “In [18], the inverse optimal adaptive control law combing adaptive control approach and optimal control method is designed to solve the attitude tracking problem of a rigid spacecraft.”