2015
DOI: 10.1108/aeat-12-2012-0258
|View full text |Cite
|
Sign up to set email alerts
|

Robust control of a yaw-pitch gimballed seeker

Abstract: If you would like to write for this, or any other Emerald publication, then please use our Emerald for Authors service information about how to choose which publication to write for and submission guidelines are available for all. Please visit www.emeraldinsight.com/authors for more information. About Emerald www.emeraldinsight.comEmerald is a global publisher linking research and practice to the benefit of society. The company manages a portfolio of more than 290 journals and over 2,350 books and book series … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
5

Citation Types

0
7
0

Year Published

2016
2016
2022
2022

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 8 publications
(7 citation statements)
references
References 27 publications
0
7
0
Order By: Relevance
“…Also, during the online simulation of this system, the Fuzzy PID controller was not able to control the entire flight path due to the complexity of applying the online conditions, and after a limited distance, the system was diverted and is not directed to the target [7]. A dynamical model of the gimballed system regarding the cross coupling unit, the angular motion platform and the input of torque disturbances for both the azimuth and elevation channel was submitted and the designer by using feedback Linearization has stabilized stability and attenuate the chaos [8]. In this paper, the dynamics of flight and simulation was not studied during various flight and engagement scenarios.…”
Section: Introductionmentioning
confidence: 99%
“…Also, during the online simulation of this system, the Fuzzy PID controller was not able to control the entire flight path due to the complexity of applying the online conditions, and after a limited distance, the system was diverted and is not directed to the target [7]. A dynamical model of the gimballed system regarding the cross coupling unit, the angular motion platform and the input of torque disturbances for both the azimuth and elevation channel was submitted and the designer by using feedback Linearization has stabilized stability and attenuate the chaos [8]. In this paper, the dynamics of flight and simulation was not studied during various flight and engagement scenarios.…”
Section: Introductionmentioning
confidence: 99%
“…In all types of homing guidance, an onboard sensor, namely a seeker, is utilized to provide target data so as to ensure target acquisition and tracking by the missile. Indeed, the seeker is the eye of a homing missile and provides LOS (line-of-sight) angular rate and the measurements of target motion including relative range and closing velocity (see literature [9][10][11] for more details).…”
Section: Introductionmentioning
confidence: 99%
“…Similarly, Yang et al 15 and Zhan et al 16 proposed different prototypes for the static unbalance measurement system. Based on Zhan and colleagues early work, 16,17 the flexure-based mechanism is proposed and acts as a bridge between the double-frame mechanism and a force sensor. Therefore, the linearity characteristics of the force transmission have significant effects on the measurement precision of this system.…”
Section: Introductionmentioning
confidence: 99%
“…Our developed static unbalance measurement system has a unique resolution of 0.0013 g cm and maximum hysteresis error of 0.12 g cm, which is superior to our early work and other conventional systems. 14,16,17,22,23 The remainder of this article is organised as follows. Section 'The static unbalance measurement system' introduces the measuring principle and the structure of the static unbalance system.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation