This paper proposes an Incremental Sliding Mode Control driven by Sliding Mode
Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant …

In order to achieve high-speed flight of a damaged quadrotor with complete loss of a single
rotor, a multiloop hybrid nonlinear controller is designed. By fully making use of sensor …

This paper describes methods to identify an integrated propulsion–airframe aerodynamic
model and a decoupled propulsion model for fixed-wing aircraft with propellers using flight …

The accuracy of dynamic modelling of unmanned aerial vehicles, specifically quadrotors, is
gaining importance since strict conditionalities are imposed on rotorcraft control. The system …

This paper proposes a systematic approach for identifying the translational dynamics of a
novel two-layer octocopter. Initially, we derive the non-linear theoretical dynamic model of …

Aerodynamic investigation of multirotor crafts under non-hover conditions plays a vital role in
the development of efficient and stable systems. Non-hover conditions include any flight …

Compared to safe obstacle avoidance in the position space, ensuring the safety of the
attitude system in today's aerial vehicle operations is more challenging due to the non …

This project reviews an accelerated proof-of-concept development technique of a novel
hybrid-lift unmanned aerial vehicle (UAV) at approximately quarter scale, encompassing the …

View Video Presentation: https://doi. org/10.2514/6.2023-0296. vid Naval aviators use
tethers to assist rotorcraft during ship board landing because of the ability to increase …

Electric multirotor air vehicles have become a pervasive technology and research topic in
industry, academia, and daily life, and small quadrotors are one of the most preferred …