2021
DOI: 10.3390/s21093084
|View full text |Cite
|
Sign up to set email alerts
|

Star Identification Based on Multilayer Voting Algorithm for Star Sensors

Abstract: This paper describes the multilayer voting algorithm, a novel autonomous star identification method for spacecraft attitude determination. The proposed algorithm includes two processes: an initial match process and a verification process. In the initial match process, a triangle voting scheme is used to acquire candidates of the detected stars, in which the triangle unit is adopted as the basic voting unit. During the identification process, feature extraction is implemented, and each triangle unit is describe… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
5
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
7

Relationship

2
5

Authors

Journals

citations
Cited by 12 publications
(5 citation statements)
references
References 30 publications
0
5
0
Order By: Relevance
“…We use the discretization mathematical idea to set the temperature control conditions as the small grid temperature matrix, as shown in Figure 6. We obtain the set temperature gradient matrix (∆T 0-row ) by decomposing the set temperature conditions and calculate the actual temperature gradient matrix (∆T row ) from the actual temperature matrix, for example, the row direction temperature gradient matrix as shown in Equation (10).…”
Section: Conversion Algorithm For Thermal Conditionsmentioning
confidence: 99%
See 2 more Smart Citations
“…We use the discretization mathematical idea to set the temperature control conditions as the small grid temperature matrix, as shown in Figure 6. We obtain the set temperature gradient matrix (∆T 0-row ) by decomposing the set temperature conditions and calculate the actual temperature gradient matrix (∆T row ) from the actual temperature matrix, for example, the row direction temperature gradient matrix as shown in Equation (10).…”
Section: Conversion Algorithm For Thermal Conditionsmentioning
confidence: 99%
“…However, the evaluation of thermal deformation currently relies pri ulation analysis and lacks direct testing of object deformation. Several un Similarly, in the calibration of star sensors, the thermal deformation frame of the dome-type multi-star simulator (Figure 3) significantly impac simulation accuracy of the simulator [9][10][11][12]. By identifying the thermal d rection of the support frame, timely correction of the thermal deformation prove the simulation accuracy of the star simulator.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…The star sensor is currently known as the most accurate attitude measurement instrument, and it also has the characteristics of no drift and autonomy [ 1 , 2 , 3 , 4 , 5 , 6 , 7 , 8 , 9 , 10 , 11 ]. Therefore, the star sensor has been widely used in the field of aerospace navigation [ 12 , 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 ].…”
Section: Introductionmentioning
confidence: 99%
“…1. We aimed to solve the problem of star identification over the entire sky using an autonomous recognition algorithm based on a compound calibration star grid pattern (Liu et al 2021). The main algorithm included initial matching and verification.…”
mentioning
confidence: 99%