Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Shaoping Wang"'
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
In this paper, thermal slide rheostats of cylinder and thermal circuit network based on them have been studied. The object here is abstracted from part of cylinder in swashplate axial piston pump (SAPP) in electro-hydrostatic actuator (EHA). Obviousl
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
This paper designs an active fault-tolerant controller based on Model Reference Adaptive Control (MRAC) and Linear Quadratic Regulator (LQR) for horizontal stabilizer asymmetric damaged large aircraft. Defining the parameters of damaged horizontal st
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
This paper proposes a novel nonlinear controller for path following control of underactuated autonomous underwater vehicle (AUV) in the horizon plane. In order to overcome the drawback of dependence on the accurate dynamic model that are present in a
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
This paper focuses on statistic method under small test samples through re-sampling for aeronautics pump. Based on the limit accelerated life testing samples and regular life testing samples, this paper presents a life evaluation method combing the S
Autor:
Xuesong Luo, Shaoping Wang
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
The gaps between permanent magnets are inevitable in linear oscillating motor because of the manufacturing process, which are ignored in the past research. The objective of this paper is to study the influence of gaps on magnetic field. A modified an
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
In order to realize condition-based maintenance of aircraft and therefore ensure flight safety, it is significant to timely and accurately determine of remaining useful life (RUL) of the aviation hydraulic piston pump. Failure resulting from hydrauli
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
As civil aircrafts require high requirement of reliability, the flight control system should make airplane safe at least when failure occurs. This paper proposed an active fault-tolerant control (AFTC) strategy for civil aircraft with ailerons stuck
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS).
The iron bird is a kind of “iron bird environment” which includes many auxiliary test benches and experimental devices. This thesis describes the main features, the definition of modular design and design process of modern aircraft iron bird. Mod
Publikováno v:
2016 IEEE International Conference on Aircraft Utility Systems (AUS); 2016, p768-773, 6p