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A novel method for computing state transition matrices due to the unscented transform.
Rahil Makadia1, Davide Farnocchia2, Steven R Chesley2
1Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, 104 S. Wright St., Urbana, IL 61801 USA.
We developed a novel unscented transform method for nonlinear dynamical systems. This approach simplifies calculations by avoiding derivatives and arbitrary steps, matching traditional performance.
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Area of Science:
- Dynamical Systems and Control Theory
- Astrodynamics and Spaceflight Mechanics
- Computational Mathematics
Background:
- State transition matrices are crucial for analyzing nonlinear dynamical systems.
- Traditional methods like finite differences involve complex derivatives or arbitrary step sizes.
- Accurate propagation of uncertainty is essential in many scientific and engineering applications.
Purpose of the Study:
- To introduce a new, simplified method for computing state transition matrices for nonlinear dynamical systems.
- To eliminate the need for complex partial derivatives and arbitrary perturbation steps.
- To evaluate the performance and accuracy of the proposed method in diverse applications.
Main Methods:
- The proposed method utilizes the unscented transform to compute state transition matrices.
- It avoids explicit computation of Jacobian matrices and auto-differentiation.
- The method was tested on a two-body problem, Mars atmospheric entry, and asteroid close encounters.
Main Results:
- The unscented transform state transition matrices were shown to preserve symplecticity.
- Performance was comparable to classical unscented transform methods.
- The new method accurately reproduced posterior distributions from Monte Carlo simulations, even with stiff dynamics.
Conclusions:
- The proposed unscented transform method offers a robust and simplified alternative for computing state transition matrices in nonlinear systems.
- It maintains accuracy and desirable properties like symplecticity.
- This method has broad applicability in astrodynamics, flight mechanics, and other fields involving complex dynamics.