Modeling Considerations for Developing Deep Space Autonomous Spacecraft and Simulators

被引:0
|
作者
Agia, Christopher [1 ]
Vila, Guillem Casadesus [2 ]
Bandyopadhyay, Saptarshi [3 ]
Bayard, David S. [3 ]
Cheung, Kar-Ming [3 ]
Lee, Charles H. [3 ]
Wood, Eric [3 ]
Aenishanslin, Ian [4 ]
Ardito, Steven [3 ]
Fesq, Lorraine [3 ]
Pavone, Marco [2 ]
Nesnas, Issa A. D. [3 ]
机构
[1] Stanford Univ, Dept Comp Sci, Stanford, CA 94305 USA
[2] Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
[3] CALTECH, Jet Prop Lab, Pasadena, CA 91125 USA
[4] Inst Polytech Sci Avancees, Ivry, France
基金
美国国家航空航天局;
关键词
FLEXIBLE SPACECRAFT; ATTITUDE ESTIMATION; NAVIGATION; STABILIZATION; GUIDANCE; DESIGN; FIELD; DRAG;
D O I
10.1109/AERO58975.2024.10521055
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Over the last two decades, space exploration systems have incorporated increasing levels of onboard autonomy to perform mission-critical tasks in time-sensitive scenarios or to bolster operational productivity for long-duration missions. Such systems use models of spacecraft subsystems and the environment to enable the execution of autonomous functions (functional-level autonomy) within limited time windows and/or with constraints. These models and constraints are carefully crafted by experts on the ground and uploaded to the spacecraft via prescribed safe command sequences for the spacecraft to execute. Such practice is limited in its efficacy for scenarios that demand greater operational flexibility. To extend the limited scope of autonomy used in prior missions for operation in distant and complex environments, there is a need to further develop and mature autonomy that jointly reasons over multiple subsystems, which we term system-level autonomy. System-level autonomy establishes situational awareness that resolves conflicting information across subsystems, which may necessitate the refinement and interconnection of the underlying spacecraft and environment onboard models. However, with a limited understanding of the assumptions and tradeoffs of modeling to arbitrary extents, designing onboard models to support system-level capabilities presents a significant challenge. For example, simple onboard models that exclude cross-subsystem effects may compromise the efficacy of an autonomous spacecraft, while complex models that capture interdependencies among spacecraft subsystems and the environment may be infeasible to simulate under the real-world operating constraints of the spacecraft (e.g., limited access to spacecraft and environment states, and computational resources). In this paper, we provide a detailed analysis of the increasing levels of model fidelity for several key spacecraft subsystems, with the goal of informing future spacecraft functional- and system-level autonomy algorithms and the physics-based simulators on which they are validated. We do not argue for the adoption of a particular fidelity class of models but, instead, highlight the potential tradeoffs and opportunities associated with the use of models for onboard autonomy and in physics-based simulators at various fidelity levels. We ground our analysis in the context of deep space exploration of small bodies, an emerging frontier for autonomous spacecraft operation in space, where the choice of models employed onboard the spacecraft may determine mission success. We conduct our experiments in the Multi-Spacecraft Concept and Autonomy Tool (MuSCAT), a software suite for developing spacecraft autonomy algorithms.
引用
收藏
页数:20
相关论文
共 50 条
  • [21] Autonomous Navigation for Deep Spacecraft Based on Celestial Objects
    Song, Min
    Yuan, Yunbin
    2008 2ND INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1 AND 2, 2008, : 812 - 815
  • [22] Radiometric Spacecraft Tracking for Deep Space Navigation
    Lanyi, Gabor E.
    Border, James S.
    Shin, Dong K.
    PROCEEDINGS OF THE 2008 NATIONAL TECHNICAL MEETING OF THE INSTITUTE OF NAVIGATION - NTM 2008, 2008, : 86 - 90
  • [23] Virtual Lidar Sensor Intensity Data Modeling for Autonomous Driving Simulators
    Lee, Dong-Ju
    Im, Jiung
    Won, Jong-Hoon
    IEEE ACCESS, 2023, 11 : 120694 - 120706
  • [24] Spacecraft to Spacecraft Absolute Tracking for Autonomous Navigation of a Distributed Space System from Relative Sensors
    Greaves, Jesse
    Scheeres, Daniel
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2024, 71 (05):
  • [25] Application of AF-NUMIT2 to the Modeling of Deep-Dielectric Spacecraft Charging in the Space Environment
    Beecken, Brian P.
    Englund, Joel T.
    Lake, Jonathan J.
    Wallin, Bryan M.
    IEEE TRANSACTIONS ON PLASMA SCIENCE, 2015, 43 (09) : 2817 - 2827
  • [26] Spacecraft transponder for deep space applications: Design and performance
    Simone, L
    Comparini, MC
    Marchetti, F
    D'Attilia, M
    Cocchi, S
    Delfino, M
    Delfino, A
    Basile, G
    De Tiberis, F
    Boscagli, G
    2002 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOLS 1-7, 2002, : 1337 - 1347
  • [27] Deep space 1 spacecraft vibration qualification testing
    Chang, KY
    SOUND AND VIBRATION, 2001, 35 (03): : 14 - 17
  • [28] Radiation environment onboard spacecraft at LEO and in deep space
    Sihver, L.
    Kodaira, S.
    Ambrozova, I.
    Uchihori, Y.
    Shurshakov, V.
    2016 IEEE AEROSPACE CONFERENCE, 2016,
  • [29] Novel Deep Space Nuclear Electric Propulsion Spacecraft
    Howe, Troy
    Howe, Steve
    Miller, Jack
    NUCLEAR TECHNOLOGY, 2021, 207 (06) : 866 - 875
  • [30] Deep Space 1 spacecraft vibration qualification testing
    Chang, Kurng Y.
    S V Sound and Vibration, 2001, 35 (03): : 14 - 17