In-flight attitude perturbances estimation: application to PLEIADES-HR satellites

Amberg, V.; Dechoz, Cécile; Bernard, Laurent; Greslou, D.; Lussy, F. de; Lebègue, Laurent

doi:10.1117/12.2023275

Cited by 34 publications

(24 citation statements)

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…The attitude perturbance, which is commonly induced by the dynamic structure on board, the changes in the body temperature, the operation of the orbital control, and so on, is a universal problem occurring in the flight of earth observation satellites (Amberg et al, 2013;Johnston and Thornton, 2000;Takaku and Tadono, 2010;Iwasaki, 2011). With the increase of spatial resolution and the enhancement of maneuverability, the attitude perturbance of the satellite platform has made a crucial impact upon geometric performance of high resolution satellite images (HRSI) (Liu et al, 2011;Mattson et al, 2009;Poli et al, 2014).…”

Section: Introductionmentioning

confidence: 99%

“…With the increase of spatial resolution and the enhancement of maneuverability, the attitude perturbance of the satellite platform has made a crucial impact upon geometric performance of high resolution satellite images (HRSI) (Liu et al, 2011;Mattson et al, 2009;Poli et al, 2014). With the help of the commonly used high resolution CCD linear array sensors, the attitude perturbance can be effectively extracted from the HRSI obtained by an imaging system with parallax observation (Amberg et al, 2013;Iwasaki, 2011). Some successful application has already been conducted on typical observation satellites such as High Resolution Imaging Science Experiment (HiRISE) (Mattson et al, 2009), Lunar Reconnaissance Orbiter (LRO) (Mattson et al, 2010;Mattson et al, 2011), Terra (Iwasaki, 2011), SPOT 5 (Latry andDelvit, 2009), Pleiades-HR (Amberg et al, 2013).…”

Section: Introductionmentioning

confidence: 99%

“…With the help of the commonly used high resolution CCD linear array sensors, the attitude perturbance can be effectively extracted from the HRSI obtained by an imaging system with parallax observation (Amberg et al, 2013;Iwasaki, 2011). Some successful application has already been conducted on typical observation satellites such as High Resolution Imaging Science Experiment (HiRISE) (Mattson et al, 2009), Lunar Reconnaissance Orbiter (LRO) (Mattson et al, 2010;Mattson et al, 2011), Terra (Iwasaki, 2011), SPOT 5 (Latry andDelvit, 2009), Pleiades-HR (Amberg et al, 2013). Compared with the typical approaches, the methods of parallax observation seem to be more economically and technically feasible for many on-orbit satellites.…”

Section: Introductionmentioning

confidence: 99%

See 2 more Smart Citations

Estimation of the Attitude Perturbance Using Parallax Imagery - Application to Zy-3 Satellite

Wang

et al. 2015

ISPRS Ann. Photogramm. Remote Sens. Spatial Inf. Sci.

View full text Add to dashboard Cite

ABSTRACT:The inflight stability of the earth observation satellite is a significant factor having an influence on the geometric performance of its imagery. The estimation of the attitude perturbance is therefore indispensable to spaceborne photogrammetry application. In this paper, an experiment using a short strip of multispectral images obtained from ZY-3 satellite is conducted. The detection method for attitude perturbance based on parallax observation is adopted, while a novel approach of estimating the attitude perturbance angles from the perturbance caused image displacements is also proposed and demonstrated. The estimated results indicate that the ZY-3 satellite was affected by considerable perturbances with distinctive frequencies during the flight of the investigated images, and attitude perturbances hava also undermined the geometric performance of the acquired imagery.

show abstract

Section: Introductionmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Estimation of the Attitude Perturbance Using Parallax Imagery - Application to Zy-3 Satellite

Wang

et al. 2015

ISPRS Ann. Photogramm. Remote Sens. Spatial Inf. Sci.

View full text Add to dashboard Cite

show abstract

“…However, those methods that depend on accurate GCPs or high-performance attitude sensors are economically and technically infeasible for many on-orbit satellites. For such reasons, a number of studies have been carried out to detect and analyze attitude jitter based on imagery, provided attitude data, RPCs and products such as digital elevation model (DEM) and orthoimages [3,[13][14][15][16][17][18][19][20].…”

Section: Introductionmentioning

confidence: 99%

“…They succeeded in acquiring the frequency and amplitude of jitter. Furthermore, using the parallax formed by neighbouring multispectral sensors, Amberg et al detected the attitude micro-vibration of PLEIADES-HR satellite without the help of additional devices [15].…”

Section: Introductionmentioning

confidence: 99%

Framework of Jitter Detection and Compensation for High Resolution Satellites

Tong

et al. 2014

Remote Sensing

View full text Add to dashboard Cite

Attitude jitter is a common phenomenon in the application of high resolution satellites, which may result in large errors of geo-positioning and mapping accuracy. Therefore, it is critical to detect and compensate attitude jitter to explore the full geometric potential of high resolution satellites. In this paper, a framework of jitter detection and compensation for high resolution satellites is proposed and some preliminary investigation is performed. Three methods for jitter detection are presented as follows. (1) The first one is based on multispectral images using parallax between two different bands in the image; (2) The second is based on stereo images using rational polynomial coefficients (RPCs); (3) The third is based on panchromatic images employing orthorectification processing. Based on the calculated parallax maps, the frequency and amplitude of the detected jitter are obtained. Subsequently, two approaches for jitter compensation are conducted. (1) The first one is to conduct the compensation on image, which uses the derived parallax observations for resampling; (2) The second is to conduct the compensation on attitude data, which treats the influence of jitter on attitude as correction of charge-coupled device (CCD) viewing angles. Experiments with images from several satellites, such as ASTER (Advanced Spaceborne Thermal Emission and Reflection Radiaometer), LRO (Lunar Reconnaissance 3945Orbiter) and ZY-3 (ZiYuan-3) demonstrate the promising performance and feasibility of the proposed framework.

show abstract