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arxiv: 2604.19539 · v1 · submitted 2026-04-21 · ⚛️ physics.geo-ph

Recognition: unknown

An effective window framework for closed-Loop regional SAR reconnaissance with hybrid direct-relay downlink scheduling

Authors on Pith no claims yet

Pith reviewed 2026-05-10 00:52 UTC · model grok-4.3

classification ⚛️ physics.geo-ph
keywords SAR reconnaissanceobservation window generationimaging quality screeningback-projection imaginghybrid direct-relay schedulingclosed-loop MILPregional SAR planning
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The pith

The framework generates SAR observation windows to millisecond timing accuracy, screens them for imaging quality with point-target back-projection, and solves a hybrid direct-relay MILP to increase closed-loop data return.

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

The paper develops an integrated window framework that first produces geometrically feasible candidate observation intervals for regional SAR using angular bandpass screening, a planar curve containment test, and one-dimensional boundary bisection. Each surviving window is then evaluated in stripmap mode by simulating a companion point target under a unified echo generation and back-projection workflow; only those meeting preset thresholds on impulse response width, peak sidelobe ratio, and integrated sidelobe ratio are kept. The retained windows feed a quality-constrained mixed-integer linear program that jointly schedules observations and hybrid direct-relay downlinks. A sympathetic reader would care because operational success requires simultaneous satisfaction of geometry, image quality, and timely ground delivery rather than visibility alone. Numerical tests show millisecond agreement with STK reference timings and measurable gains in closure performance and returned data volume over a relay-only baseline.

Core claim

Through coarse angular bandpass screening, a planar characteristic curve containment test, and one-dimensional boundary bisection, the framework forms geometry-feasible candidate observation windows with millisecond-level accuracy for entry and exit times; each window is assessed with a companion point target under unified echo generation and back-projection imaging so that only those whose range and azimuth IRW, PSLR, and ISLR satisfy preset thresholds are retained; the retained windows then enter a quality-constrained hybrid direct-relay closed-loop MILP that jointly schedules observation and ground return.

What carries the argument

The effective window framework that chains angular bandpass screening, planar characteristic curve containment, one-dimensional boundary bisection for timing, point-target back-projection quality screening on IRW/PSLR/ISLR, and a quality-constrained hybrid direct-relay MILP scheduler.

If this is right

  • Window boundary times agree with STK reference at the millisecond level.
  • Only windows whose range and azimuth impulse response widths, peak sidelobe ratios, and integrated sidelobe ratios meet preset thresholds are retained for scheduling.
  • The hybrid direct-relay closed-loop MILP improves both closure performance and total ground-returned data volume compared with a relay-only baseline.

Where Pith is reading between the lines

These are editorial extensions of the paper, not claims the author makes directly.

  • The same screening and scheduling structure could be tested on other SAR modes such as spotlight or scanSAR by swapping the echo-generation module while keeping the MILP intact.
  • Replacing the single point-target companion with a small set of distributed point targets or a low-resolution extended scene inside the screening step would directly test robustness to real target complexity.
  • Embedding a fast heuristic or warm-start solver for the MILP could further reduce latency if operational planners need sub-second replanning cycles.

Load-bearing premise

That screening each candidate window against a single companion point target under a unified echo generation and back-projection workflow is sufficient to predict imaging quality for real extended targets and that the resulting MILP can be solved fast enough for operational closed-loop use without unmodeled platform errors or atmospheric effects.

What would settle it

A side-by-side comparison of the quality metrics (IRW, PSLR, ISLR) obtained from the point-target screening workflow versus the same metrics measured on actual extended-target imagery collected in the identical windows, or a timing benchmark of the MILP solver on representative operational hardware that includes realistic platform jitter and atmospheric delays.

Figures

Figures reproduced from arXiv: 2604.19539 by Kebo Li, Linhong Li, Qi Feng, Yangang Liang.

Figure 1
Figure 1. Figure 1: Overall view of the mission closure problem. [PITH_FULL_IMAGE:figures/full_fig_p004_1.png] view at source ↗
Figure 2
Figure 2. Figure 2: STK side looking SAR parameter panel used to define the elevation and Doppler constraints. [PITH_FULL_IMAGE:figures/full_fig_p010_2.png] view at source ↗
Figure 3
Figure 3. Figure 3: Geometric components of the coarse angular screening. [PITH_FULL_IMAGE:figures/full_fig_p012_3.png] view at source ↗
Figure 4
Figure 4. Figure 4: SAR field of view as an annular envelope on the ground plane (a) and as an analytic boundary on the VVLH calculation plane (b). [PITH_FULL_IMAGE:figures/full_fig_p013_4.png] view at source ↗
Figure 5
Figure 5. Figure 5: Nine ordered configurations of the admissible domain [PITH_FULL_IMAGE:figures/full_fig_p014_5.png] view at source ↗
Figure 6
Figure 6. Figure 6: Three complementary geometric tests for the polygon domain intersection predicate (67). [PITH_FULL_IMAGE:figures/full_fig_p015_6.png] view at source ↗
Figure 7
Figure 7. Figure 7: Schematic of bisection refinement for coarse boundary brackets. [PITH_FULL_IMAGE:figures/full_fig_p018_7.png] view at source ↗
Figure 8
Figure 8. Figure 8: Schematic definitions of the three point target quality indicators. [PITH_FULL_IMAGE:figures/full_fig_p019_8.png] view at source ↗
Figure 9
Figure 9. Figure 9: Comparison of scheduling results of the two methods in a Gantt chart. [PITH_FULL_IMAGE:figures/full_fig_p025_9.png] view at source ↗
Figure 10
Figure 10. Figure 10: STK reference scenario used in Experiment II. [PITH_FULL_IMAGE:figures/full_fig_p027_10.png] view at source ↗
Figure 11
Figure 11. Figure 11: Time histories used in the coarse angular screening. [PITH_FULL_IMAGE:figures/full_fig_p028_11.png] view at source ↗
Figure 12
Figure 12. Figure 12: VVLH calculation plane projections at the entry and exit instants of Window 1. [PITH_FULL_IMAGE:figures/full_fig_p028_12.png] view at source ↗
Figure 13
Figure 13. Figure 13: Refined predicate decomposition over two candidate intervals. [PITH_FULL_IMAGE:figures/full_fig_p029_13.png] view at source ↗
Figure 14
Figure 14. Figure 14: Time varying observation geometry within the three candidate windows. [PITH_FULL_IMAGE:figures/full_fig_p031_14.png] view at source ↗
Figure 15
Figure 15. Figure 15: Sentinel-2C L2A optical basemap over central Beijing. [PITH_FULL_IMAGE:figures/full_fig_p032_15.png] view at source ↗
Figure 16
Figure 16. Figure 16: Reprojected truth maps and multi look BP images for W0 to W2. [PITH_FULL_IMAGE:figures/full_fig_p033_16.png] view at source ↗
Figure 17
Figure 17. Figure 17: STK 2D ground track view of the Experiment IV scenario at the mission epoch. [PITH_FULL_IMAGE:figures/full_fig_p034_17.png] view at source ↗
Figure 18
Figure 18. Figure 18: Experiment IV: Gantt chart of the 24 hour schedule. [PITH_FULL_IMAGE:figures/full_fig_p036_18.png] view at source ↗
read the original abstract

For operational regional synthetic aperture radar (SAR) reconnaissance, mission success depends not only on geometric visibility but also on whether geometric feasibility, prescribed imaging quality, and timely data delivery can be met together within the planning horizon. This paper develops an effective window framework for regional SAR window generation, per window signal level quality screening, and hybrid direct-relay closed loop scheduling. Through coarse angular bandpass screening, a planar characteristic curve containment test, and one dimensional boundary bisection, the framework forms geometry feasible candidate observation windows with millisecond-level accuracy for their entry and exit times. Each candidate window is then assessed in stripmap mode with a companion point target under a unified echo generation and Back Projection (BP) imaging workflow; only windows whose range and azimuth impulse response width (IRW), peak sidelobe ratio (PSLR), and integrated sidelobe ratio (ISLR) all satisfy the preset thresholds are retained. The retained observation, relay, and downlink windows feed a quality constrained hybrid direct-relay closed-loop mixed-integer linear programming (MILP) formulation for joint scheduling of observation and ground return. Numerical experiments confirm millisecond-level agreement with STK reference timing for window boundaries. Every candidate window is screened against preset imaging quality thresholds. Hybrid closed-loop scheduling improves closure performance and ground returned data volume relative to a relay-only baseline

Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, simulated authors' rebuttal, and a circularity audit. Tearing a paper down is the easy half of reading it; the pith above is the substance, this is the friction.

Referee Report

2 major / 1 minor

Summary. The manuscript develops an effective window framework for closed-loop regional SAR reconnaissance. It generates geometrically feasible observation windows via coarse angular bandpass screening, planar characteristic curve containment, and 1D boundary bisection (millisecond entry/exit accuracy), screens each candidate in stripmap mode against a companion point target using unified echo generation and back-projection to enforce IRW/PSLR/ISLR thresholds, and feeds the retained windows into a quality-constrained hybrid direct-relay MILP scheduler for joint observation and downlink optimization. Numerical experiments are reported to confirm STK timing agreement and performance gains over a relay-only baseline.

Significance. If the point-target proxy and MILP scalability hold under operational conditions, the integrated treatment of geometry, per-window quality, and hybrid scheduling would be a practical advance for SAR mission planning, enabling higher data return while respecting imaging constraints. The explicit relay-only baseline comparison and preset (non-fitted) quality thresholds are strengths.

major comments (2)
  1. [Quality screening procedure] The per-window quality screening (abstract and methods description) retains candidates solely if a single companion point target imaged in stripmap mode satisfies preset IRW, PSLR, and ISLR thresholds. For regional reconnaissance the actual scene is extended; no validation, sensitivity study, or comparison against distributed scatterers is provided to show that these point-target metrics predict usable image quality, which is load-bearing for both the retained-window set and the subsequent scheduling improvement claim.
  2. [Numerical experiments] Numerical experiments (abstract) claim millisecond-level STK agreement and improved closure/data volume, yet no quantitative metrics (timing RMSE, data-volume deltas, scenario count, or sensitivity to platform/atmospheric errors) or baseline implementation details are supplied in the provided text, leaving the central performance assertions only partially supported.
minor comments (1)
  1. The abstract would be strengthened by including at least one key quantitative result (e.g., timing error or data-volume improvement percentage) rather than qualitative statements.

Simulated Author's Rebuttal

2 responses · 0 unresolved

We thank the referee for the constructive and detailed comments, which help clarify the strengths and limitations of our framework. We address each major comment below and indicate the revisions planned for the next manuscript version.

read point-by-point responses
  1. Referee: [Quality screening procedure] The per-window quality screening (abstract and methods description) retains candidates solely if a single companion point target imaged in stripmap mode satisfies preset IRW, PSLR, and ISLR thresholds. For regional reconnaissance the actual scene is extended; no validation, sensitivity study, or comparison against distributed scatterers is provided to show that these point-target metrics predict usable image quality, which is load-bearing for both the retained-window set and the subsequent scheduling improvement claim.

    Authors: The point-target proxy in stripmap mode was selected for computational efficiency when screening the large set of geometrically feasible candidate windows produced by the angular bandpass and boundary bisection steps. The preset IRW/PSLR/ISLR thresholds follow standard SAR imaging specifications to enforce basic resolvability and sidelobe control. We acknowledge that the manuscript does not contain a dedicated validation, sensitivity study, or direct comparison against distributed scatterers for extended regional scenes, which limits the strength of the claim that retained windows guarantee usable image quality in operational settings. In the revised manuscript we will add a dedicated subsection in the methods or discussion that (i) justifies the proxy choice with references to prior SAR literature, (ii) explicitly states its limitations for distributed targets, and (iii) outlines how future work could incorporate extended-scene metrics. This addition will not alter the core screening procedure but will better contextualize its applicability. revision: yes

  2. Referee: [Numerical experiments] Numerical experiments (abstract) claim millisecond-level STK agreement and improved closure/data volume, yet no quantitative metrics (timing RMSE, data-volume deltas, scenario count, or sensitivity to platform/atmospheric errors) or baseline implementation details are supplied in the provided text, leaving the central performance assertions only partially supported.

    Authors: We agree that the current presentation of the numerical experiments is insufficiently quantitative. Although the abstract summarizes the outcomes, the full manuscript text does not report explicit values such as timing RMSE, numerical data-volume or closure deltas, the exact number of scenarios, or sensitivity results. In the revised version we will expand the numerical experiments section to include: (i) timing RMSE and maximum deviation figures for the STK comparison, (ii) concrete data-volume and closure-performance deltas with the relay-only baseline, (iii) the number and diversity of scenarios tested, (iv) any sensitivity checks performed with respect to platform or atmospheric errors, and (v) additional implementation details for the baseline scheduler. These additions will be supported by updated tables or figures as appropriate. revision: yes

Circularity Check

0 steps flagged

No circularity: framework uses independent geometric tests, preset thresholds, and explicit baseline comparison

full rationale

The derivation proceeds via explicit geometric screening (angular bandpass, planar curve containment, bisection), point-target quality checks against fixed IRW/PSLR/ISLR thresholds, and MILP scheduling whose performance gain is measured directly against a relay-only baseline. Window timing is cross-checked against external STK software rather than self-referential data. No equation or claim reduces to a fitted parameter renamed as prediction, no self-citation supplies a load-bearing uniqueness result, and no ansatz is smuggled in. The pipeline is therefore self-contained against external benchmarks.

Axiom & Free-Parameter Ledger

0 free parameters · 2 axioms · 0 invented entities

The central claim rests on the accuracy of standard geometric containment tests, the representativeness of point-target BP simulation for operational image quality, and the fidelity of the MILP model to real scheduling constraints. No new physical entities are introduced and no parameters are fitted to data within the abstract.

axioms (2)
  • domain assumption Point-target back-projection simulation with preset IRW/PSLR/ISLR thresholds accurately predicts imaging quality for real extended targets.
    Invoked when retaining or discarding candidate windows after echo generation.
  • domain assumption The mixed-integer linear program correctly captures all operational constraints on observation, relay, and downlink timing.
    Required for the closed-loop scheduling step to produce feasible and optimal plans.

pith-pipeline@v0.9.0 · 5542 in / 1584 out tokens · 92026 ms · 2026-05-10T00:52:38.935026+00:00 · methodology

discussion (0)

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Reference graph

Works this paper leans on

53 extracted references · 40 canonical work pages

  1. [1]

    Bensana, G

    E. Bensana, G. Verfaillie, J. Agnese, N. Bataille, D. Blumstein, Earth observation satellite management, Constraints 4 (3) (1999) 293–311. doi:10.1023/A:1026488509554

  2. [2]

    W. J. Wolfe, S. E. Sorensen, Three scheduling algorithms applied to the earth observing systems domain, Management Science 46 (1) (2000) 148–168. doi:10.1287/mnsc.46.1.148.15134

  3. [3]

    Lema ˆıtre, G

    M. Lema ˆıtre, G. Verfaillie, F. Jouhaud, J.-M. Lachiver, N. Bataille, Selecting and scheduling observations of agile satellites, Aerospace Science and Technology 6 (8) (2002) 537–550. doi:10.1016/S1270-9638(02)01173-2

  4. [4]

    Bianchessi, J.-F

    N. Bianchessi, J.-F. Cordeau, G. Desaulniers, G. Laporte, V . Raymond, A heuristic for the multi-satellite, multi-orbit and multi-user manage- ment of earth observation satellites, European Journal of Operational Research 177 (2) (2007) 750–762. doi:10.1016/j.ejor.2005.12.026

  5. [5]

    X. Liu, B. Bai, Y . Chen, B. Alidaee, F. Glover, An adaptive large neighborhood search metaheuristic for agile satellite scheduling with time-dependent transition time, Computers & Operations Research 86 (2017) 48–59. doi:10.1016/j.cor.2017.04.006

  6. [6]

    Y . She, Y . Xu, Y . Zhao, Onboard mission planning for agile satellite using modified mixed-integer linear programming, Aerospace Science and Technology 72 (2018) 204–216. doi:10.1016/j.ast.2017.11.009

  7. [7]

    X. Chen, G. Reinelt, G. Dai, A. Spitz, A mixed integer linear programming model for multi-satellite scheduling, European Journal of Operational Research 275 (2) (2019) 694–707. doi:10.1016/j.ejor.2018.11.058

  8. [8]

    M. Wang, C. Han, A. Zhao, Y . Xu, Task scheduling and attitude planning for agile earth observation satellite with intensive tasks, Aerospace Science and Technology 90 (2019) 24–32. doi:10.1016/j.ast.2019.04.007

  9. [9]

    G. Peng, M. Dessouky, Z. Wei, An exact algorithm for agile earth observation satellite scheduling with time-dependent profits, Computers & Operations Research 120 (2020) 104946. doi:10.1016/j.cor.2020.104946

  10. [10]

    G. Peng, J. Wang, G. Song, A. Gunawan, L. Xing, P. Vansteenwegen, Branch-and-cut-and-price for agile earth observation satellite schedul- ing, European Journal of Operational Research 326 (3) (2025) 427–438. doi:10.1016/j.ejor.2025.04.014

  11. [11]

    X. Wang, G. Wu, L. Xing, W. Pedrycz, Agile earth observation satellite scheduling over 20 years: Formulations, methods, and future directions, IEEE Systems Journal 15 (3) (2021) 3881–3892. doi:10.1109/JSYST.2020.2997050

  12. [12]

    J. Chen, M. Chen, J. Wen, L. He, X. Liu, A heuristic construction neural network method for the time-dependent agile earth observation satellite scheduling problem, Mathematics 10 (19) (2022) 3498. doi:10.3390/math10193498

  13. [13]

    Y . Feng, R. Zhang, S. Ren, S. Zhu, Y . Yang, A distributed approach for time-dependent observation scheduling problem in the agile earth observation satellite constellation, Remote Sensing 15 (7) (2023) 1761. doi:10.3390/rs15071761

  14. [14]

    Krigman, T

    S. Krigman, T. Grinshpoun, L. Dery, Scheduling of earth observing satellites using distributed constraint optimization, Journal of Scheduling 27 (2024) 507–524. doi:10.1007/s10951-024-00816-x

  15. [15]

    Rojanasoonthon, J

    S. Rojanasoonthon, J. F. Bard, Algorithms for parallel machine scheduling: A case study of the tracking and data relay satellite system, Journal of the Operational Research Society 54 (5) (2003) 480–494. doi:10.1057/palgrave.jors.2601575

  16. [16]

    Karapetyan, S

    D. Karapetyan, S. Mitrovic-Minic, K. T. Malladi, A. P. Punnen, Satellite downlink scheduling problem: A case study, Omega 53 (2015) 115–123. doi:10.1016/j.omega.2015.01.001

  17. [17]

    Spangelo, J

    S. Spangelo, J. Cutler, K. Gilson, A. Cohn, Optimization-based scheduling for the single-satellite, multi-ground station communication problem, Computers & Operations Research 57 (2015) 1–16. doi:10.1016/j.cor.2014.11.004

  18. [18]

    X.-j. Hu, X. Luo, X. Zhang, M. Wang, A branch and price algorithm for EOS constellation imaging and downloading integrated scheduling problem, Computers & Operations Research 104 (2019) 193–204. doi:10.1016/j.cor.2018.12.007

  19. [19]

    Zhang, N

    Z. Zhang, N. Zhang, X. Luan, An improved genetic algorithm for the integrated satellite imaging and data transmission scheduling problem, Computers & Operations Research 139 (2022) 105626. doi:10.1016/j.cor.2021.105626

  20. [20]

    G. Yu, K. Zhang, Research on the integrated scheduling of imaging and data transmission for earth observation satellites, Algorithms 18 (7) (2025) 418. doi:10.3390/a18070418

  21. [21]

    Y . He, J. Li, W. Li, et al., Dynamic scheduling of hybrid tasks with time windows in data relay satellite networks, IEEE Transactions on Vehicular Technology 68 (5) (2019) 4989–5003. doi:10.1109/TVT.2019.2903737

  22. [22]

    J. Chen, X. Dia, R. Xu, H. Qi, L. Cong, K. Zhang, Z. Xing, X. He, W. Lei, S. Zhang, A remote sensing data transmission strategy based on the combination of satellite-ground link and geo relay under dynamic topology, Future Generation Computer Systems 145 (2023) 337–353. doi:10.1016/j.future.2023.02.016

  23. [23]

    C. He, Y . Dong, Multi-satellite observation-relay transmission-downloading coupling scheduling method, Remote Sensing 15 (24) (2023)

  24. [24]

    doi:10.3390/rs15245639

  25. [25]

    S. J. Kim, M. Kim, C.-H. Kim, H.-L. Choi, Satellite scheduling framework of observation-relay-downlink with a mixed-integer linear pro- gramming model, in: AIAA SCITECH 2025 Forum, 2025. doi:10.2514/6.2025-2273

  26. [26]

    S. J. Kim, M. Kim, C.-H. Kim, H.-L. Choi, Integrated earth observation satellite scheduling with relay-assisted downlink, Aerospace Science and Technology 168 (2026) 110864. doi:10.1016/j.ast.2025.110864

  27. [27]

    J. J. Morrison, A system of sixteen synchronous satellites for worldwide navigation and surveillance, Tech. rep., Federal Aviation Adminis- tration, Systems Research and Development Service, Washington, D.C. (1973)

  28. [28]

    R. G. Casten, R. P. Gross, Satellite cumulative earth coverage, in: AIAA Astrodynamics Specialist Conference, Lake Tahoe, Nevada, 1981

  29. [29]

    Middour, An efficient technique for computation of satellite earth coverage, in: Proceedings of the 27th AIAA Aerospace Sciences Meeting, Washington, D.C., 1989

    J. Middour, An efficient technique for computation of satellite earth coverage, in: Proceedings of the 27th AIAA Aerospace Sciences Meeting, Washington, D.C., 1989

  30. [30]

    J. A. Lawton, Numerical method for rapidly determining satellite-satellite and satellite-ground station in-view periods, Journal of Guidance, Control, and Dynamics 10 (1) (1987) 32–36. 39 Author et al./Aerospace Science and Technology 00 (2026) 1–4040

  31. [31]

    Alfano, D

    S. Alfano, D. Negron, J. L. Moore, Rapid determination of satellite visibility periods, Journal of the Astronautical Sciences 40 (2) (1992) 281–296

  32. [32]

    Y . Mai, P. Palmer, Fast algorithm for prediction of satellite imaging and communication opportunities, Journal of Guidance, Control, and Dynamics 24 (6). doi:10.2514/2.4846

  33. [33]

    Sun, et al., APCHI technique for rapidly and accurately predicting multi-restriction satellite visibility, in: Proc

    X. Sun, et al., APCHI technique for rapidly and accurately predicting multi-restriction satellite visibility, in: Proc. Twenty-Second AAS/AIAA Space Flight Mechanics Meeting, Charleston, South Carolina, 2012

  34. [34]

    C. Han, X. Gao, X. Sun, Rapid satellite-to-site visibility determination based on self-adaptive interpolation technique, Science China Tech- nological Sciences 60 (2) (2017) 264–270. doi:10.1007/s11431-016-0513-8

  35. [35]

    H. Wang, C. Han, X. Sun, Analytical field-of-regard representation for rapid and accurate prediction of agile satellite imaging opportunities, Journal of Astronomical Telescopes, Instruments, and Systems 5 (3) (2019) 037001. doi:10.1117/1.JATIS.5.3.037001

  36. [36]

    Nugnes, C

    M. Nugnes, C. Circi, M. Massari, Coverage area determination for conical fields of view considering an oblate earth, Journal of Guidance, Control, and Dynamics 42 (10) (2019) 2233–2245. doi:10.2514/1.G004156

  37. [37]

    M. Zuo, G. Dai, L. Peng, An envelope curve-based theory for the satellite coverage problems, Aerospace Science and Technology 100 (2020) 105750. doi:10.1016/j.ast.2020.105750

  38. [38]

    C. Han, Y . Zhang, S. Bai, X. Sun, X. Wang, Novel method to calculate satellite visibility for an arbitrary sensor field, Aerospace Science and Technology 112 (2021) 106668. doi:10.1016/j.ast.2021.106668

  39. [39]

    Jiang, S

    Y . Jiang, S. Bai, H. Wang, Minimum-observation method for rapid and accurate satellite coverage prediction, GPS Solutions 26 (4) (2022)

  40. [40]

    doi:10.1007/s10291-022-01295-3

  41. [41]

    H. Wang, S. Bai, A versatile method for target area coverage analysis with arbitrary satellite attitude maneuver paths, Acta Astronautica 194 (2022) 242–254. doi:10.1016/j.actaastro.2022.02.008

  42. [42]

    Zhang, Z

    Z. Zhang, Z. E, L. Huang, J. Li, Semi-analytical algorithm for computing satellite-area target visibility, Journal of Tsinghua University (Science and Technology) 62 (3) (2022) 573–580. doi:10.16511/j.cnki.qhdxxb.2021.26.020

  43. [43]

    Y . Gu, X. Sun, L. Fan, S. Liu, G. Wu, A rapid satellite-ground coverage analysis method based on elevation view element model, Acta Aeronautica et Astronautica Sinica 45 (23) (2024) 330372. doi:10.7527/S1000-6893.2024.30372

  44. [44]

    Y . Shan, C. Du, Y . Li, Z. Li, X. Jin, H. Zhang, Triple time interval hybridization strategy for rapidly calculating regional target–visible time window of earth observation payloads on space station, Applied Sciences 14 (6) (2024) 2388. doi:10.3390/app14062388

  45. [45]

    X. Shi, W. Xing, H. Liu, Y . Wang, M. Xing, Vtwsar: A fast calculation method for visible time window of sar satellite to regional target, IEEE Journal of Selected Topics in Applied Earth Observations and Remote Sensing 18 (2025) 14063–14075. doi:10.1109/JSTARS.2025.3574518

  46. [46]

    J. C. Curlander, R. N. McDonough, Synthetic Aperture Radar: Systems and Signal Processing, John Wiley & Sons, New York, 1991

  47. [47]

    I. G. Cumming, F. H. Wong, Digital Processing of Synthetic Aperture Radar Data: Algorithms and Implementation, Artech House, Norwood, MA, 2005

  48. [48]

    H. Li, J. An, X. Jiang, M. Lin, Raw data simulation of spaceborne synthetic aperture radar with accurate range model, Remote Sensing 15 (11) (2023) 2705. doi:10.3390/rs15112705

  49. [49]

    H. Li, J. An, X. Jiang, Accurate range modeling for high-resolution spaceborne synthetic aperture radar, Sensors 24 (10) (2024) 3119. doi:10.3390/s24103119

  50. [50]

    D. A. Vallado, Fundamentals of Astrodynamics and Applications, 4th Edition, Microcosm Press, Hawthorne, CA, 2013

  51. [51]

    D. A. Vallado, P. Crawford, R. Hujsak, T. S. Kelso, Revisiting spacetrack report #3, in: AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Keystone, CO, 2006. doi:10.2514/6.2006-6753

  52. [52]

    O’Rourke, Computational Geometry in C, Cambridge University Press, Cambridge, UK, 1994

    J. O’Rourke, Computational Geometry in C, Cambridge University Press, Cambridge, UK, 1994

  53. [53]

    ANSYS, Inc., STK Ephemeris File Format (.e),https://help.agi.com/stk/Content/stk/importfiles-02.htm, sTK external ephemeris file specification; accessed 2026-04-19 (2025). 40