Citation
Malhotra, Sunil K. (1992) Nonlinear uncertainty propagation in space trajectories. Engineer's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd08092007085505
Abstract
This thesis addresses the problem of nonlinear uncertainty propagation in space trajectories. This problem can be specifically stated as follows: Given the initial orbital state of a spacecraft trajectory as random variables, what is the orbital state at some later time? This problem is currently encountered by mission designers at institutions such as the Jet Propulsion Laboratory. Before an expensive space probe is irretrievably launched, extensive trajectory analyses are conducted to determine the amount of fuel needed to correct for trajectory errors. This involves propagation of uncertainties in the trajectories. The current method for uncertainty propagation involves linearizing about the nominal trajectory to obtain a state transition matrix used to map the covariance matrix to a later orbital state. This method neglects nonlinear effects. Two new algorithms were developed to account for nonlinear effects in the propagation of uncertainties in space trajectories. The first utilized simplifying assumptions to obtain analytic expressions for the probabilistic quantities describing the final orbital state. This algorithm provided good trend information but lacked precision. The second algorithm utilized Gaussian quadrature techniques to numerically compute the desired quantities. While requiring significant computational effort, this algorithm provided high precision. Example trajectories were analyzed to compare the results from the new algorithms to those from the current method. Nonlinear effects were shown to influence both the mean and the variance results.
Item Type:  Thesis (Engineer's thesis) 

Degree Grantor:  California Institute of Technology 
Major Option:  Mechanical Engineering 
Thesis Availability:  Public (worldwide access) 
Thesis Committee: 

Defense Date:  15 May 1992 
Record Number:  CaltechETD:etd08092007085505 
Persistent URL:  http://resolver.caltech.edu/CaltechETD:etd08092007085505 
Default Usage Policy:  No commercial reproduction, distribution, display or performance rights in this work are provided. 
ID Code:  3076 
Collection:  CaltechTHESIS 
Deposited By:  Imported from ETDdb 
Deposited On:  14 Aug 2007 
Last Modified:  22 Aug 2016 21:16 
Thesis Files

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