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在“tasks/heading_task.py”文件中,delta_heading属性为目标偏航角与自身偏航角的差值,而在“test/test_baseline_use_env.py”文件中,PursueAgent类set_delta_value成员函数中采用的是北天东坐标系,在水平面的速度向量与LOS向量的夹角作为delta_heading。 训练时,您在“termination_conditions/unreach_heading.py”中将目标偏航角设置为期望航向,希望飞机自身通过改变偏航角与期望航向吻合。然而在测试时,您将目标方位作为期望航向,但是似乎希望飞机自身通过改变水平面速度方向与期望航向吻合,而速度方向与机身纵轴方向在6DOF模型中一般是不重合的(jsbsim中同样是6DOF,是否应该考虑因迎角和侧滑角带来的差异?)
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在“tasks/heading_task.py”文件中,delta_heading属性为目标偏航角与自身偏航角的差值,而在“test/test_baseline_use_env.py”文件中,PursueAgent类set_delta_value成员函数中采用的是北天东坐标系,在水平面的速度向量与LOS向量的夹角作为delta_heading。
训练时,您在“termination_conditions/unreach_heading.py”中将目标偏航角设置为期望航向,希望飞机自身通过改变偏航角与期望航向吻合。然而在测试时,您将目标方位作为期望航向,但是似乎希望飞机自身通过改变水平面速度方向与期望航向吻合,而速度方向与机身纵轴方向在6DOF模型中一般是不重合的(jsbsim中同样是6DOF,是否应该考虑因迎角和侧滑角带来的差异?)
The text was updated successfully, but these errors were encountered: