2017
DOI: 10.1002/asjc.1571
|View full text |Cite
|
Sign up to set email alerts
|

Three‐Dimensional Impact Angle Constrained Guidance Laws with Fixed‐Time Convergence

Abstract: In this paper, three dimensional coupled engagement dynamics are firstly transformed into a state-space form without decoupling three dimensional engagement dynamics into two mutually orthogonal planes to avoid degrading the performance of the guidance law. Specially, fixed-time guidance laws are proposed to guarantee that the line-of-sight (LOS) angular rates can be steered to zero before the final time of the guidance process at the same time. The exact convergence time can be set beforehand with respect to … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
11
0

Year Published

2019
2019
2021
2021

Publication Types

Select...
6
1

Relationship

0
7

Authors

Journals

citations
Cited by 15 publications
(11 citation statements)
references
References 33 publications
0
11
0
Order By: Relevance
“…Then the three-dimensional relative kinematic dynamics between missile and target can be expressed as follows [27]:…”
Section: Missile-target Interception Geometrymentioning
confidence: 99%
See 1 more Smart Citation
“…Then the three-dimensional relative kinematic dynamics between missile and target can be expressed as follows [27]:…”
Section: Missile-target Interception Geometrymentioning
confidence: 99%
“…The objective of the guidance law is to achieve the interception of missile and target, with desired impact angle and . The impact angle is defined to be the LOS angles as in [27] [28]. As nullifying the LOS angular rates ̇ and ̇ can lead to the interception, the solution to this problem is to design the missile accelerations to guarantee the following equations: ̇ = ̇ = 0, = , = .…”
Section: Missile-target Interception Geometrymentioning
confidence: 99%
“…Taking the longitudinal plane as an example, the missile impact angle θ d is defined as the included angle between the missile and the target velocity vectors at the engagement time, and the impact angle corresponds to the terminal LOS angle as follows [20,21]:…”
Section: Problem Formulationmentioning
confidence: 99%
“…Line-of-sight (LOS) angles are denoted by θ L and φ L . Then the three-dimensional engagement dynamics can be expressed as follows [41]:…”
Section: In This Figure O I X I Y I Z I O M X M Y M Z M and O T mentioning
confidence: 99%