Robust distributed sensor fault detection and diagnosis within formation control of multiagent systems
This article investigates the fault detection and diagnosis (FDD) problem for multiagent
systems subject to sensor faults and disturbances. A distributed proportional integral …
systems subject to sensor faults and disturbances. A distributed proportional integral …
[HTML][HTML] Pseudospectral-Based Rapid Trajectory Planning and Feedforward Linearization Guidance
A trajectory-based guidance strategy is proposed for the three-dimensional terminal return
task of an uncrewed space vehicle (USV). The overall guidance scheme consists of …
task of an uncrewed space vehicle (USV). The overall guidance scheme consists of …
Composite Attitude Tracking Control for Launch Vehicles Subject to Actuator Degradation Fault and Multiple Disturbances
H Teng, Y Zhu, J Qiao, X Yao… - IEEE Transactions on …, 2024 - ieeexplore.ieee.org
The safety and high-precision attitude control of launch vehicles are threatened by
degradation fault and multiple disturbances (such as model uncertainty, uncertain inertia …
degradation fault and multiple disturbances (such as model uncertainty, uncertain inertia …
Fast Prediction of Reachable Area for Reusable Vehicle under Waypoint Constrains using a Multiobjective DRL Heuristic Algorithm
H Zhou, X Wang, R Liu, N Cui - IEEE Transactions on Vehicular …, 2024 - ieeexplore.ieee.org
A reachable area defines the potential end positions that a reusable vehicle can reach
under its current flight state. The area comprises feasible flight trajectories and helps to …
under its current flight state. The area comprises feasible flight trajectories and helps to …
Three-Dimensional Ascent Guidance Method for Two-Stage Solid Rocket Launch Vehicles under Multiple Constraints and Uncertainties
This article proposes a new three-dimensional (3D) guidance algorithm for a two-stage solid
rocket-powered launch vehicle in the ascent phase. The method consists of a longitudinal …
rocket-powered launch vehicle in the ascent phase. The method consists of a longitudinal …
Counterfactual Negative Outcome Control for Required Navigation Performance
T Yin - 2023 China Automation Congress (CAC), 2023 - ieeexplore.ieee.org
Output feedback control in flight relies on robust guidance commands. However, inevitable
command deviations can result in excessive and adverse servo adjustments of the aircraft …
command deviations can result in excessive and adverse servo adjustments of the aircraft …
Fast Trajectory Optimization for Reusable Launch Vehicle Using Multiple Analytical Solutions and an Adaptive Noise Maximum Entropy Reinforcement Learning …
H Zhou, X Wang, R Liu, C Naigang - Available at SSRN 4895890 - papers.ssrn.com
Online trajectory optimization is of critical importance to the reusable launch vehicle in
emergency return cases. However, deriving the optimal trajectory instantaneously is …
emergency return cases. However, deriving the optimal trajectory instantaneously is …