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Particle steering problem: Difference between revisions

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|nx        = 2
|nx        = 2
|nw        = 1
|nw        = 1
|nc        = 2
|nre      = 7
|nre      = 7
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}}<!-- Do not insert line break here or Dimensions Box moves up in the layout...
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  & \ddot{x}_1 & = & a \cos (u), \\
  & \ddot{x}_1 & = & a \cos (u), \\
  & \ddot{x}_2 & = & a \sin (u),  \\
  & \ddot{x}_2 & = & a \sin (u),  \\
  & x(t_0) &=& (0, 0)^T, \\
  & x(0) &=& (0, 0)^T, \\
  & \dot{x}(0) &=& (0, 0)^T, \\
  & \dot{x}(0) &=& (0, 0)^T, \\
  & x_2 (t_f) &=& 5, \\
  & x_2 (t_f) &=& 5, \\
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[[Category:MIOCP]]
[[Category:MIOCP]]
[[Category:ODE model]]
[[Category:ODE model]]
[[Category:Minimum time]]

Latest revision as of 08:33, 27 July 2016

Particle steering problem
State dimension: 1
Differential states: 2
Discrete control functions: 1
Path constraints: 2
Interior point equalities: 7

The Particle steering problem minimizes "the time taken for a particle, acted upon by a thrust of constant magnitude, to achieve a given altitude and terminal velocity." (Cite and problem taken from the COPS library)


Mathematical formulation

The problem is given by

minx,u,tftfs.t.x¨1=acos(u),x¨2=asin(u),x(0)=(0,0)T,x˙(0)=(0,0)T,x2(tf)=5,x˙(tf)=(45,0)T,u(t)[π2,π2].


where (x1,x2) is the position of the particle, u is the control angle and a is the constant magnitude of thrust.

Source Code

Model descriptions are available in