A Sampled-Data Form of Incremental Nonlinear Dynamic Inversion for Spacecraft Attitude Control

Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

Quadrotor fault-tolerant incremental nonsingular terminal sliding mode control

Incremental Sliding-Mode Fault-Tolerant Flight Control

Quadrotor Fault Tolerant Incremental Sliding Mode Control driven by Sliding Mode Disturbance Observers

Flight testing of incremental backstepping based control laws with angular accelerometer feedback

Stability Analysis for Incremental Nonlinear Dynamic Inversion Control

Comparison of three control structures for inducing higher-order sliding modes

Safe Exploration Algorithms for Reinforcement Learning Controllers

Machine Learning for Flapping Wing Flight Control

Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

Stability Analysis for Incremental Nonlinear Dynamic Inversion Control

Stability and Robustness Analysis and Improvements for Incremental Nonlinear Dynamic Inversion Control

Robust Incremental Nonlinear Dynamic Inversion Control Using Angular Accelerometer Feedback

Design and flight testing of incremental nonlinear dynamic inversion based control laws for a passenger aircraft

Effects of structural failure on the safe flight envelope of aircraft

Adaptive spacecraft attitude control with incremental approximate dynamic programming

Gust Load Alleviation and Ride Quality Improvement with Incremental Nonlinear Dynamic Inversion

Nonlinear adaptive flight control using incremental approximate dynamic programming and output feedback

Framework for Simultaneous Sensor and Actuator Fault-Tolerant Flight Control