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26 March 2026

  • 09:4209:42, 26 March 2026 Three Tank OED (hist | edit) [4,422 bytes] RobertLampel (talk | contribs) (Created page with "{{Dimensions |nd = 1 |nx = 21 |nw = 6 }} The '''Three Tank OED problem''' is a variation of the Three Tank multimode problem. It looks for optimal time intervals to measure the two states in order to minimize the uncertainty of a follow-up parameter estimation problem for the two unknown parameters. The mathematical equations form a small-scale ODE model. It also includes state sensitivities, the Fisher information matr...")
  • 08:3908:39, 26 March 2026 Lotka Shared OED (hist | edit) [5,286 bytes] RobertLampel (talk | contribs) (Created page with "{{Dimensions |nd = 1 |nx = 11 |nw = 2 |nc = 4 |nre = 11 }} The '''Lotka Shared Experimental Design problem''' looks for an optimal strategy to be performed on a fixed time horizon to control the biomasses multiple species as described in LV Shared Resource. The goal here, however, is to minimize the uncertainty of a follow-up parameter estimation problem. When measurements of the three state variables are performed becomes a degree...")

3 February 2026

  • 08:1508:15, 3 February 2026 Cart Pendulum (hist | edit) [3,088 bytes] RobertLampel (talk | contribs) (Created page with "{{Dimensions |nd = 1 |nx = 3 |nw = 2 }} The '''Cart Pendulum problem''' concerns a pendulum hinged to a mobile cart. The control objective is to transition the pendulum from a downward position to a stabilized, inverted state above the cart. In this formulation, the objective function is defined by a composite of least-squares terms. The implementation here is taken from [1]. Its dynamics are given by a four-dimensional :Category:...")
  • 07:5107:51, 3 February 2026 Moon Landing (hist | edit) [1,676 bytes] RobertLampel (talk | contribs) (Created page with "{{Dimensions |nd = 1 |nx = 3 |nw = 2 }} The '''Moon Landing problem''' is a simplification of a spacecraft trying to land on the moon's surface. Its objective is to minimize the fuel consumption during the landing maneuver while landing savely on the ground with zero vertical velocity. The implementation here is taken from [1]. Its dynamics are given by a two-dimensional ODE model. == Mathematical formulatio...")

27 January 2026

  • 07:3107:31, 27 January 2026 Jackson OED (hist | edit) [4,319 bytes] RobertLampel (talk | contribs) (Created page with "{{Dimensions |nd = 1 |nx = 13 |nw = 3 }} The '''Jackson OED problem''' is a variation of the Jackson problem. It looks for optimal time intervals to measure the three states in order to minimize the uncertainty of a follow-up parameter estimation problem for the two unknown parameters. The mathematical equations form a small-scale ODE model. It also includes state sensitivities, the Fisher information matrix entries and...")

26 January 2026