The next generation of reentry vehicles is envisioned to have onboard autonomous capability of real-time trajectory planning to provide capability of responsive launch and delivering payload anywhere with precise flight termination. This capability is also desired to overcome, if possible, in-flight vehicle damage or control effector failure resulting in degraded vehicle performance. An aerial vehicle is modeled as a nonlinear multi-input-multi-output (MIMO) system. An ideal optimal trajectory control design system generates a series of control commands to achieve a desired trajectory under various disturbances and vehicle model uncertainties including aerodynamic perturbations caused by geometric damage to the vehicle. Conventional approac...
We present a new neural architecture which imbeds dynamic programming solutions to solve optimal tar...
This report presents a neural-aided controller that enhances the fault tolerant high performance fig...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...
Traditional reentry dynamics and planning has typically explored 3 Degrees-of- Freedom (3 DOF) or ps...
In this thesis, the optimal control of a hypersonic vehicle in ascent through the atmosphere is deve...
Reusable Launch Vehicles (RLVs) are the future of the space industry due to their low cost and relia...
This paper describes an integrated neural flight and propulsion control system, which uses a neural ...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
We propose a methodology for extending the applicability of multibody-based comprehensive analysis c...
Optimal entry flight of hypersonic vehicles requires achieving specific mission objectives under com...
Reconfigurable inner-loop control laws improve the fault tolerance of a vehicle to control effector ...
An optimal guidance law for a missile flight is one which determines appropriate controls to produce...
This paper addresses the issue of developing a computerized system for processing information in the...
This paper presents a neural network assisted entry guidance law that is designed by applying Bézier...
Abstract—The paper presents neural dynamic optimization (NDO) as a method of optimal feedback contro...
We present a new neural architecture which imbeds dynamic programming solutions to solve optimal tar...
This report presents a neural-aided controller that enhances the fault tolerant high performance fig...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...
Traditional reentry dynamics and planning has typically explored 3 Degrees-of- Freedom (3 DOF) or ps...
In this thesis, the optimal control of a hypersonic vehicle in ascent through the atmosphere is deve...
Reusable Launch Vehicles (RLVs) are the future of the space industry due to their low cost and relia...
This paper describes an integrated neural flight and propulsion control system, which uses a neural ...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
We propose a methodology for extending the applicability of multibody-based comprehensive analysis c...
Optimal entry flight of hypersonic vehicles requires achieving specific mission objectives under com...
Reconfigurable inner-loop control laws improve the fault tolerance of a vehicle to control effector ...
An optimal guidance law for a missile flight is one which determines appropriate controls to produce...
This paper addresses the issue of developing a computerized system for processing information in the...
This paper presents a neural network assisted entry guidance law that is designed by applying Bézier...
Abstract—The paper presents neural dynamic optimization (NDO) as a method of optimal feedback contro...
We present a new neural architecture which imbeds dynamic programming solutions to solve optimal tar...
This report presents a neural-aided controller that enhances the fault tolerant high performance fig...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...