关键词:
Space stations
Algorithms
Surveillance
Space surveillance
Artificial satellites
Aerospace engineering
Computer science
Engineering
摘要:
Space Situational Awareness (SSA) is an important and pressing field, as the amount of space debris is growing due to the increase in spacecraft launches. Space agencies like NASA and ESA keep track of over 5,000 spacecraft and 20,000 spacecraft-related debris objects currently orbiting the Earth. These spacecraft may undergo trajectory changes through artificial impulsive maneuvers without warning, posing a risk to other spacecraft in the vicinity. Additionally, measurement data often consists of uncertainties, where usual spacecraft maneuver detection and characterisation methods are often computationally expensive. The goal of this work is to develop a quick, reliable, computationally inexpensive method for spacecraft maneuver detection and characterisation, which would be used to assist satellite operators in collision avoidance measures. This dissertation utilises such a technique, which is applied to simulated measurement data of an orbiting spacecraft taken from one ground site. With these objectives, a method using a modified Extended Kalman Filter (EKF) with covariance inflation from previous research was explored and simplified. Through building on this set of research, a new parameter definition is presented for maneuver detection and characterisation, named K, with focus on transverse apogee and perigee maneuvers. A relationship was then found between the detection parameter (both the original parameter, Ψ, and the new parameter, K) and the magnitude of the impulsive artificial maneuver. The detection and characterisation method was tested in several different scenarios, varying ∆v magnitude and scale, ∆v direction, maneuver orbital location, orbit geometry, noise covariance, detection parameter threshold, state covariance inflation threshold, and maneuver duration. In general, it was found that as the ∆v magnitude increases, so does the magnitude of the detection parameter. This relationship was found to be nonlinear, of either a quadratic (Ψ) or logari