In this paper, the composite robust control problem of uncertain nonlinear systems with
unmatched disturbances is investigated. In order to improve the robust control performance …

This paper investigates the design of an attitude autopilot for a dual-channel controlled
spinning glide-guided projectile (SGGP), addressing model uncertainties and external …

In this paper, a neuroadaptive high-order fully-actuated system approach control scheme
incorporating the disturbance observer technique is proposed for the missile roll autopilot …

In the human-in-loop (HIL) guidance mode, a pilot quickly identifies and flexibly locks on to a
target through a real-time image signal transmitted by the aircraft. Then, the line-of-sight …

This paper considers the problem of unmanned aerial vehicle (UAV) aerial collision net
recovery in a three-dimensional non-decoupling environment and approach angle …

In this paper, a novel fuzzy disturbance observer (DOB) is designed for a class of nonlinear
single-input–single-output (SISO) systems. The main feature of the proposed DOB lies in …

In this paper, we derive the sufficient and necessary stability conditions for rolling missiles
with velocity orientation autopilot. For the mathematical derivation, linear time-invariant …

This paper presents a new robust composite nonlinear feedback control law for accurate,
smooth, and fast regulation in the presence of parameter uncertainties, external …

The angle‐of‐attack (AOA) three‐loop feedback autopilot is an improved three‐loop
autopilot that has been widely employed in missile control systems. For spinning missiles …

Tactical missiles are used against various aerial/ground targets which can be stationary or
maneuvering. Tactical missiles should have highly efficient control scheme in order to …