Use CLARABEL solver for rocket landing optimization#1209
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Switched the solver from ECOS to CLARABEL in the optimization process of the rocket-powered landing module. This change is expected to improve performance and compatibility with specific problem constraints.
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AerialNavigation/rocket_powered_landing/rocket_powered_landing.py
| @@ -32,7 +32,7 @@ | |||
| W_NU = 1e5 # virtual control | |||
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| print(cvxpy.installed_solvers()) | |||
| @@ -32,7 +32,7 @@ | |||
| W_NU = 1e5 # virtual control | |||
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| print(cvxpy.installed_solvers()) | |||
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AerialNavigation/rocket_powered_landing/rocket_powered_landing.py
| max_angle = 90 | ||
| glidelslope_angle = 20 | ||
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| self.tan_delta_max = np.tan(np.deg2rad(max_gimbal)) |
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AerialNavigation/rocket_powered_landing/rocket_powered_landing.py
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AerialNavigation/rocket_powered_landing/rocket_powered_landing.py
| self.t_f_guess = 10.0 # 10 s | ||
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| # State constraints | ||
| self.r_I_final = np.array((0., 0., 0.)) |
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AerialNavigation/rocket_powered_landing/rocket_powered_landing.py
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Switched the solver from ECOS to CLARABEL in the optimization process of the rocket-powered landing module.
Ref
#1207
oxfordcontrol/Clarabel.rs#172
Reference issue
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