| Directory: | ./ |
|---|---|
| File: | bindings/python/crocoddyl/multibody/actuations/multicopter-base.cpp |
| Date: | 2025-03-13 15:22:42 |
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| Lines: | 24 | 25 | 96.0% |
| Branches: | 21 | 42 | 50.0% |
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| 1 | /////////////////////////////////////////////////////////////////////////////// | ||
| 2 | // BSD 3-Clause License | ||
| 3 | // | ||
| 4 | // Copyright (C) 2019-2023, LAAS-CNRS, University of Edinburgh, IRI: CSIC-UPC | ||
| 5 | // Heriot-Watt University | ||
| 6 | // Copyright note valid unless otherwise stated in individual files. | ||
| 7 | // All rights reserved. | ||
| 8 | /////////////////////////////////////////////////////////////////////////////// | ||
| 9 | |||
| 10 | #include "crocoddyl/multibody/actuations/multicopter-base.hpp" | ||
| 11 | |||
| 12 | #include "python/crocoddyl/multibody/multibody.hpp" | ||
| 13 | #include "python/crocoddyl/utils/copyable.hpp" | ||
| 14 | |||
| 15 | namespace crocoddyl { | ||
| 16 | namespace python { | ||
| 17 | |||
| 18 | 10 | void exposeActuationModelMultiCopterBase() { | |
| 19 | bp::register_ptr_to_python< | ||
| 20 | 10 | std::shared_ptr<crocoddyl::ActuationModelMultiCopterBase> >(); | |
| 21 | |||
| 22 |
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10 | bp::class_<ActuationModelMultiCopterBase, bp::bases<ActuationModelAbstract> >( |
| 23 | "ActuationModelMultiCopterBase", | ||
| 24 | "Actuation models with base actuated by several propellers (e.g. aerial " | ||
| 25 | "manipulators).", | ||
| 26 |
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10 | bp::init<std::shared_ptr<StateMultibody>, |
| 27 | Eigen::Matrix<double, 6, Eigen::Dynamic> >( | ||
| 28 | 20 | bp::args("self", "state", "tau_f"), | |
| 29 | "Initialize the full actuation model.\n\n" | ||
| 30 | ":param state: state of multibody system\n" | ||
| 31 | ":param tau_f: matrix that maps rotors thrust to generalized torque " | ||
| 32 | "of the flying base.")) | ||
| 33 |
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10 | .def(bp::init<std::shared_ptr<StateMultibody>, std::size_t, |
| 34 | Eigen::Matrix<double, 6, Eigen::Dynamic> >( | ||
| 35 |
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20 | bp::args("self", "state", "nrotors", "tau_f"), |
| 36 | "Initialize the full actuation model.\n\n" | ||
| 37 | ":param state: state of multibody system, \n" | ||
| 38 | ":param nrotors: number of rotors of the flying base, \n" | ||
| 39 | ":param tau_f: matrix that maps rotors thrust to generalized torque " | ||
| 40 | "of the flying base.")) | ||
| 41 | .def<void (ActuationModelMultiCopterBase::*)( | ||
| 42 | const std::shared_ptr<ActuationDataAbstract>&, | ||
| 43 | const Eigen::Ref<const Eigen::VectorXd>&, | ||
| 44 |
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10 | const Eigen::Ref<const Eigen::VectorXd>&)>( |
| 45 | "calc", &ActuationModelMultiCopterBase::calc, | ||
| 46 |
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20 | bp::args("self", "data", "x", "u"), |
| 47 | "Compute the actuation signal and actuation set from the joint " | ||
| 48 | "torque input u.\n\n" | ||
| 49 | ":param data: multicopter-base actuation data\n" | ||
| 50 | ":param x: state point (dim. state.nx)\n" | ||
| 51 | ":param u: joint torque input (dim. nu)") | ||
| 52 |
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10 | .def("calcDiff", &ActuationModelMultiCopterBase::calcDiff, |
| 53 |
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20 | bp::args("self", "data", "x", "u"), |
| 54 | "Compute the derivatives of the actuation model.\n\n" | ||
| 55 | "It computes the partial derivatives of the full actuation. It " | ||
| 56 | "assumes that calc\n" | ||
| 57 | "has been run first. The reason is that the derivatives are " | ||
| 58 | "constant and\n" | ||
| 59 | "defined in createData. The Hessian is constant, so we don't write " | ||
| 60 | "again this value.\n" | ||
| 61 | ":param data: multicopter-base actuation data\n" | ||
| 62 | ":param x: state point (dim. state.nx)\n" | ||
| 63 | ":param u: joint torque input (dim. nu)") | ||
| 64 |
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10 | .def("commands", &ActuationModelMultiCopterBase::commands, |
| 65 |
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20 | bp::args("self", "data", "x", "tau"), |
| 66 | "Compute the joint torque commands from the generalized torques.\n\n" | ||
| 67 | "It stores the results in data.u.\n" | ||
| 68 | ":param data: actuation data\n" | ||
| 69 | ":param x: state point (dim. state.nx)\n" | ||
| 70 | ":param tau: generalized torques (dim state.nv)") | ||
| 71 |
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10 | .def("torqueTransform", &ActuationModelMultiCopterBase::torqueTransform, |
| 72 |
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20 | bp::args("self", "data", "x", "tau"), |
| 73 | "Compute the torque transform from generalized torques to joint " | ||
| 74 | "torque inputs.\n\n" | ||
| 75 | "It stores the results in data.Mtau.\n" | ||
| 76 | ":param data: actuation data\n" | ||
| 77 | ":param x: state point (dim. state.nx)\n" | ||
| 78 | ":param tau: generalized torques (dim state.nv)") | ||
| 79 |
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10 | .def("createData", &ActuationModelMultiCopterBase::createData, |
| 80 |
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20 | bp::args("self"), |
| 81 | "Create the multicopter-base actuation data.\n\n" | ||
| 82 | "Each actuation model (AM) has its own data that needs to be " | ||
| 83 | "allocated.\n" | ||
| 84 | "This function returns the allocated data for a predefined AM.\n" | ||
| 85 | ":return AM data.") | ||
| 86 |
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10 | .add_property( |
| 87 | "nrotors", | ||
| 88 |
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20 | bp::make_function(&ActuationModelMultiCopterBase::get_nrotors), |
| 89 | "Number of rotors in the flying base") | ||
| 90 |
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10 | .add_property( |
| 91 | "tauf", | ||
| 92 |
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10 | bp::make_function(&ActuationModelMultiCopterBase::get_tauf, |
| 93 | ✗ | bp::return_value_policy<bp::return_by_value>()), | |
| 94 |
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20 | bp::make_function(&ActuationModelMultiCopterBase::set_tauf), |
| 95 | "Matrix mapping from thrusts to body torque") | ||
| 96 |
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10 | .def(CopyableVisitor<ActuationModelMultiCopterBase>()); |
| 97 | 10 | } | |
| 98 | |||
| 99 | } // namespace python | ||
| 100 | } // namespace crocoddyl | ||
| 101 |