Optimal morphing–augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies

I Mir, A Maqsood, SA Eisa, H Taha, S Akhtar - Aerospace Science and …, 2018 - Elsevier
This paper investigates autonomous dynamic soaring maneuvers for a small Unmanned
Aerial Vehicle (sUAV) having the capability to morph. Dynamic soaring for UAVs have …

Optimal control of a formula one car on a three-dimensional track—Part 2: Optimal control

DJN Limebeer, G Perantoni - Journal of …, 2015 - asmedigitalcollection.asme.org
The optimal control of a Formula One car on a three-dimensional (3D) track is studied. The
track is described by its geodesic and normal curvatures, and its relative torsion. These …

Optimal tyre usage for a Formula One car

AJ Tremlett, DJN Limebeer - Vehicle System Dynamics, 2016 - Taylor & Francis
Variations in track temperature, surface conditions and layout have led tyre manufacturers to
produce a range of rubber compounds for race events. Each compound has unique friction …

[HTML][HTML] Suboptimal LQR-based spacecraft full motion control: Theory and experimentation

L Guarnaccia, R Bevilacqua, SP Pastorelli - Acta Astronautica, 2016 - Elsevier
This work introduces a real time suboptimal control algorithm for six-degree-of-freedom
spacecraft maneuvering based on a State-Dependent-Algebraic-Riccati-Equation (SDARE) …

Biologically inspired dynamic soaring maneuvers for an unmanned air vehicle capable of sweep morphing

I Mir, A Maqsood, S Akhtar - … Journal of Aeronautical and Space Sciences, 2018 - Springer
Dynamic soaring is a versatile maneuver executed to acquire energy available in the
atmospheric wind shears. In this paper, an innovative concept of integrating wing sweep …

A trajectory design method for coupling aircraft radar cross-section characteristics

Q Xu, J Ge, T Yang, X Sun - Aerospace Science and Technology, 2020 - Elsevier
Fast and safe aircraft penetration is important to a battle mission. Radar is a major threat in
the process of aircraft penetration. To cope with the radar threat, a trajectory design method …

A rapid penetration trajectory optimization method for hypersonic vehicles

B Yan, R Liu, P Dai, M **ng, S Liu - International Journal of …, 2019 - Wiley Online Library
The evasion maneuver problem of hypersonic vehicles differs from those of ballistic missiles
and other traditional weapons, showing distinctive properties including expansive maneuver …

An angles-only navigation and control scheme for noncooperative rendezvous operations

Y Zhang, P Huang, K Song… - IEEE Transactions on …, 2019 - ieeexplore.ieee.org
The use of vision sensors for noncooperative rendezvous operations is attractive, especially
for microspacecraft, because vision sensors are usually of small size, light weight, and low …

Multistage launch vehicle design with thrust profile and trajectory optimization

EC Coşkun - 2014 - search.proquest.com
In the frame of this thesis, a Matlab® based design tool utilizing a general purpose optimal
control solver GPOPS-II® was developed for the optimization of ascent trajectories of …

Perpetual dynamic soaring in linear wind shear

R Bencatel, P Kabamba, A Girard - Journal of Guidance, Control, and …, 2014 - arc.aiaa.org
THIS paper analyzes dynamic soaring in linear wind shear. Wind shear is a type of space
and time-dependent airflow vector field. Dynamic soaring is a cyclic flight trajectory that …