[go: up one dir, main page]

Ronse et al., 2014 - Google Patents

Statistical impact prediction of decaying objects

Ronse et al., 2014

View PDF
Document ID
1241688435406616703
Author
Ronse A
Mooij E
Publication year
Publication venue
Journal of Spacecraft and Rockets

External Links

Snippet

This paper describes a method for statistically predicting the impact time and location of an orbital object under 200 km altitude. It also investigates the influence of the chief parameter uncertainties on the statistical dispersion. Unlike the main methods used nowadays, which …
Continue reading at www.researchgate.net (PDF) (other versions)

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in preceding groups
    • G01C21/10Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10Complex mathematical operations
    • G06F17/18Complex mathematical operations for evaluating statistical data, e.g. average values, frequency distributions, probability functions, regression analysis

Similar Documents

Publication Publication Date Title
Ronse et al. Statistical impact prediction of decaying objects
DeMars et al. Collision probability with Gaussian mixture orbit uncertainty
Wang Analysis of Debris from the Collision of the Cosmos 2251 and the Iridium 33 Satellites
McMahon et al. Improving space object catalog maintenance through advances in solar radiation pressure modeling
Sagnières et al. Long-term rotational motion analysis and comparison to observations of the inoperative Envisat
Geul et al. Analysis of uncertainties and modeling in short-term reentry predictions
Ray et al. A drag coefficient modeling approach using spatial and temporal Fourier expansions for orbit determination
Ceotto et al. RocketPy: six degree-of-freedom rocket trajectory simulator
Boone et al. Simulation of debris events in selected low lunar orbits
Dutta et al. Postflight Assessment of Mars 2020 Entry, Descent, and Landing Simulation
Hernando-Ayuso et al. Near-linear orbit uncertainty propagation using the generalized equinoctial orbital elements
Ray et al. Drag coefficient model to track variations due to attitude and orbital motion
Liu et al. Guidance and control technology of spacecraft on elliptical orbit
Kenneally High geometric fidelity solar radiation pressure modeling via graphics processing unit
Fujimoto et al. Short-arc correlation and initial orbit determination for space-based observations
Anderson et al. Methodology for characterizing high-risk orbital debris in the geosynchronous orbit regime
Majid et al. Aerodynamic Drag Computation of Lower Earth Orbit (LEO) Satellites
Van Hove et al. ExoMars flush air data system: entry simulation and atmospheric reconstruction method
Parker et al. Influences of space weather forecasting uncertainty on satellite conjunction assessment
Fitzpatrick et al. Applying energy dissipation rate GNSS accelerometry to a non‐circular orbiting satellite
Karlgaard et al. Planetary probe entry atmosphere estimation using synthetic air data system
Anderson et al. Longitude-dependent effects of fragmentation events in the geosynchronous orbit regime
Gao et al. Prediction of Orbit Decay for Large‐Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects
Berthet et al. Reverse Engineering of Perturbations in the Orbital Decay Environment from Nanosatellite Two-Line Elements
Kerr et al. Incorporating solar activity into general perturbation analysis of atmospheric friction