Optimal entry flight of hypersonic vehicles requires achieving specific mission objectives under complex nonlinear flight dynamics constraints. The challenge lies in rapid generation of optimal or near-optimal flight trajectories with significant changes in the initial flight conditions during entry. Deep Neural Networks (DNNs) have shown the capability to capture the inherent nonlinear mapping between states and optimal actions in complex control problems. This paper focused on comprehensive investigation and evaluation of a DNN-based method for three-dimensional hypersonic entry flight trajectory generation. The network is designed using cross-validation to ensure its performance, enabling it to learn the mapping between flight states and...
Computing optimal solutions for unpowered hypersonic glide vehicle trajectories requires high degree...
International audienceIn this study a new approach is proposed for the generation of aircraft trajec...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...
In this thesis, the optimal control of a hypersonic vehicle in ascent through the atmosphere is deve...
The mission of hypersonic vehicles faces the problem of highly nonlinear dynamics and complex enviro...
This brief presents an integrated trajectory planning and attitude control framework for six-degree-...
Traditional reentry dynamics and planning has typically explored 3 Degrees-of- Freedom (3 DOF) or ps...
This paper presents a neural network assisted entry guidance law that is designed by applying Bézier...
In this paper, neural networks are trained to learn the optimal time, the initial costates, and the ...
The next generation of reentry vehicles is envisioned to have onboard autonomous capability of real-...
This paper investigates the discrete neural control for flight path angle and velocity of a generic ...
Reusable Launch Vehicles (RLVs) are the future of the space industry due to their low cost and relia...
Designing optimal feedback controllers for nonlinear dynamical systems requires solving Hamilton-Jac...
Near-pace hypersonic flight has great potential in civil and military use due to its high speed and ...
International audienceDifferential flatness, a property of some dynamic systems which has been recog...
Computing optimal solutions for unpowered hypersonic glide vehicle trajectories requires high degree...
International audienceIn this study a new approach is proposed for the generation of aircraft trajec...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...
In this thesis, the optimal control of a hypersonic vehicle in ascent through the atmosphere is deve...
The mission of hypersonic vehicles faces the problem of highly nonlinear dynamics and complex enviro...
This brief presents an integrated trajectory planning and attitude control framework for six-degree-...
Traditional reentry dynamics and planning has typically explored 3 Degrees-of- Freedom (3 DOF) or ps...
This paper presents a neural network assisted entry guidance law that is designed by applying Bézier...
In this paper, neural networks are trained to learn the optimal time, the initial costates, and the ...
The next generation of reentry vehicles is envisioned to have onboard autonomous capability of real-...
This paper investigates the discrete neural control for flight path angle and velocity of a generic ...
Reusable Launch Vehicles (RLVs) are the future of the space industry due to their low cost and relia...
Designing optimal feedback controllers for nonlinear dynamical systems requires solving Hamilton-Jac...
Near-pace hypersonic flight has great potential in civil and military use due to its high speed and ...
International audienceDifferential flatness, a property of some dynamic systems which has been recog...
Computing optimal solutions for unpowered hypersonic glide vehicle trajectories requires high degree...
International audienceIn this study a new approach is proposed for the generation of aircraft trajec...
The missed-thrust problem is a modern challenge in the field of mission design. While some methods e...