Continuation Methods and Non-Linear/Non-Gaussian Estimation for Flight Dynamics

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,994.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
NNX10CD47P
Agency Tracking Number:
095584
Solicitation Year:
n/a
Solicitation Topic Code:
O4
Solicitation Number:
n/a
Small Business Information
Numerica Corporation
4850 Hahns Peak Drive, Suite 200, Loveland, CO, 80538
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
956324362
Principal Investigator:
Randy Paffenroth
Principal Investigator
(970) 461-2000
randy.paffenroth@numerica.us
Business Contact:
Benjamin Slocumb
Business Official
(970) 612-2312
ben.slocumb@numerica.us
Research Institution:
n/a
Abstract
We propose herein to augment current NASA spaceflight dynamics programs with algorithms and software from two domains. First, we propose to use numerical parameter continuation methods to assist in computation of trajectories in complicated dynamical situations. Numerical parameter continuation methods have been used extensively to compute a menagerie of structures in dynamical systems including fixed points, periodic orbits, simple bifurcations (where the structure of the dynamics changes), Hopf bifurcations (where periodic orbits are created), invariant manifolds, hetero/homoclinic connections between invariant manifolds, etc. Perhaps more importantly for the current work, such methods have already proven their worth in flight dynamics problems, especially those having to do with the complicated dynamics near libration points. Second, we propose to use advanced filtering techniques and representations of probability density functions to appropriately compute and manage the uncertainty in the trajectories. While advanced methods for understanding and leveraging the underlying dynamics are clearly necessary for effective mission design, planning, and analysis, we contend that they do not suffice. In particular, they do not, in and of themselves, address the issue of uncertainty. Herein we discuss methods that balance the accuracy of the uncertainty representation against computational tractability, including a discussion of the notorious ``curse of dimensionality'' for problems with large state vectors. We propose approachs that revolve around modifications of algorithms such as ``log homotopy'' particle filters and especially Gaussian sum filters. Finally, we propose to integrate all of the above algorithms into standard NASA software packages GEONS, GIPSY, and GMAT.

* information listed above is at the time of submission.

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