Model-Based Soft Landing Control of an Electromechanical Engine Valve Actuator

2012 ◽  
Author(s):  
M. di Bernardo ◽  
S. Santini ◽  
A. di Gaeta ◽  
C. I. Hoyos Velasco ◽  
U. Montanaro
Keyword(s):  
Soft Landing ◽  
Engine Valve ◽  
Model Based ◽  
Landing Control

Cycle-by-Cycle Adaptive Force Compensation for the Soft-Landing Control of an Electro-Mechanical Engine Valve Actuator

2014 ◽  
Vol 17 (5) ◽  
pp. 1707-1724 ◽  
Author(s):  
Alessandro di Gaeta ◽  
Carlos I. Hoyos Velasco ◽  
Umberto Montanaro
Keyword(s):  
Soft Landing ◽  
Engine Valve ◽  
Landing Control ◽  
Force Compensation

Model-based Decoupling Control of a Magnet Engine Valve Actuator

2009 ◽  
Vol 2 (2) ◽  
pp. 254-271 ◽  
Author(s):  
Alessandro di Gaeta ◽  
Veniero Giglio ◽  
Giuseppe Police
Keyword(s):  
Decoupling Control ◽  
Engine Valve ◽  
Model Based

Model based landing control for a bistable electromagnetic actuator with discontinuous dynamics

2015 ◽  
Author(s):  
Rajan Gill ◽  
Arne Wahrburg ◽  
Octavian Craciun ◽  
Kim Listmann ◽  
Christian Reuber
Keyword(s):  
Electromagnetic Actuator ◽  
Model Based ◽  
Landing Control

D-SDRE Based Soft-Landing Control of a Lunar Lander with Active Momentum Exchange Impact Dampers

2021 ◽  
Author(s):  
Yi-Lun Hsu ◽  
Jhih-Hong Lin ◽  
Chen-Yu Chan ◽  
Cheng-Wei Chen
Keyword(s):  
Momentum Exchange ◽  
Soft Landing ◽  
Lunar Lander ◽  
Landing Control

In-flight wind identification and soft landing control for autonomous unmanned powered parafoils

2018 ◽  
Vol 49 (5) ◽  
pp. 929-946 ◽  
Author(s):  
Shuzhen Luo ◽  
Panlong Tan ◽  
Qinglin Sun ◽  
Wannan Wu ◽  
Haowen Luo ◽  
...  
Keyword(s):  
Soft Landing ◽  
Wind Identification ◽  
Landing Control

An Optimal Soft Landing Control for Moon Lander by Means of Measures

2011 ◽  
Vol 52-54 ◽  
pp. 1861-1867
Author(s):  
J.A. Fakharzadeh ◽  
Sajad Salehi
Keyword(s):  
Dynamical System ◽  
Control Strategy ◽  
Measure Space ◽  
Optimization Problem ◽  
Optimal Solution ◽  
The Other ◽  
Solution Path ◽  
Soft Landing ◽  
Variational Form ◽  
Landing Control

Designing a new control strategy for a moon lander to achieve an optimal soft landing, is the main purpose of this paper. For the dynamical system of the propeller to achieve the lowest level of fuel consumption, the problem of soft landing is presented as an optimal control one. Representing this into a variational form, transferring to an optimization problem on a measure space and then determining the optimal solution via a linear programming problem is the new solution path. This method has some important advantages in compare with the other, which are explain within a numerical simulation.

Optimal soft landing control for moon lander

Automatica ◽  
2008 ◽  
Vol 44 (4) ◽  
pp. 1097-1103 ◽  
Author(s):  
Xing-Long Liu ◽  
Guang-Ren Duan ◽  
Kok-Lay Teo
Keyword(s):  
Soft Landing ◽  
Landing Control
Sign in / Sign up

Export Citation Format

Share Document