Unmanned aerial vehicle (UAV) systems are required to independently make timely and
accurate attack and control strategies according to dynamic battlefield situations. To …

This paper proposes a time-energy efficient, artificial time delay based robust guidance
strategy with input saturation for a two-dimensional interceptor problem. A reference near …

This paper addresses the issue of a complex three-dimension (3-D) terminal guidance
process that is used against maneuvering targets while considering both the terminal impact …

Active magnetic bearings (AMB) are used to suspend the rotor freely inside the stator to
avoid any physical contact between them. Thus, it helps in significantly reducing the wear …

This work proposes a resource efficient robust control scheme for missile-target engagement
scenarios subjected to external disturbances. The robustness is achieved by using an …

In this paper, the attitude controller of spacecraft tracks the time-energy near-optimal angular
velocity generated by the Legendre Pseudospectral method (LPSM). The near-optimal …

This work proposes the use of a logarithmic quantizer to minimize the computational load on
the onboard processor of missiles. The quantizer output discretizes the continuous guidance …

Over the last few decades, the computational capabilities of the state-of-the-art processors
have increased extensively and are now capable of performing multiple parallel …

This paper proposes an automatic time-energy efficient robust control (ATERC) deployment
approach for selecting either a near-optimal closed-loop control law or a robust control law …

This paper develops a robust controller for the attitude tracking of time-energy near-optimal
angular velocity obtained by the Legendre Pseudospectral method (LPSM). The information …