Extending a risk metric for individual missions to evaluate overall risk in orbit
Wilson, Callum and Vasile, Massimiliano and Feng, Jinglang and McNally, Keiran and Maric, Nina and Horstmann, Andre (2024) Extending a risk metric for individual missions to evaluate overall risk in orbit. In: 75th International Astronautical Congress, 2024-10-14 - 2024-10-18, MICO Convention Centre.
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Abstract
Assessing the risk associated with new missions in orbit has become increasingly important. With the large number of spacecraft and debris now in orbit, there are many more close encounters between objects, which makes it more difficult to estimate the risk over the lifetime of a mission. Several approaches exist for determining the collision risk associated with a single object. This work uses a novel methodology for calculating the induced risk of a mission to define a more general measure of risk in the space environment. Risk is quantified as the product of likelihood and severity. Likelihood refers to the likelihood of a collision occurring and severity refers to the consequence of a collision. The proposed approach approximates collision likelihood between populations of objects based on the intersection of their distributions. This intersection computes the probability of the minimum orbit intersection distance between the distributions being less than a threshold distance value and scales this probability based on the number of objects. The model of severity uses data from simulated fragmentation events to model the likelihood of collisions with fragments based on parameters of the collision. These values of likelihood and severity give a risk measure for an individual object. We extend this metric to the whole environment by summing the risks associated with each object in the environment. The resulting metric considers the distribution of objects not only in altitude but also over orbital parameters of inclination and eccentricity, as well as right ascension in GEO. Example results are shown for baseline environment conditions and a range of future projected scenarios in LEO, MEO, and GEO regimes. The proposed risk metric requires assumptions on the covariance and masses of objects as well as defining the threshold distance for calculating the intersection. We further examine the effect of varying these parameters to see how different modelling assumptions would affect the metric.
ORCID iDs
Wilson, Callum ORCID: https://orcid.org/0000-0003-3736-1355, Vasile, Massimiliano ORCID: https://orcid.org/0000-0001-8302-6465, Feng, Jinglang ORCID: https://orcid.org/0000-0003-0376-886X, McNally, Keiran, Maric, Nina and Horstmann, Andre;-
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Item type: Conference or Workshop Item(Paper) ID code: 91903 Dates: DateEvent31 October 2024Published14 October 2024AcceptedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics > Astronautics. Space travel Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Strategic Research Themes > Ocean, Air and Space
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Pure Administrator Date deposited: 28 Jan 2025 15:48 Last modified: 29 Jan 2025 04:44 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/91903