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New Crowdin translations - zh-CN (#24895)
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@@ -16,9 +16,7 @@ Currently it is feeding the `manual_control_setpoint` topic directly to the actu
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To reduce control latency, the module directly polls on the gyro topic published by the IMU driver.
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<a id="airship_att_control_usage"></a>
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### 用法
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### Usage {#airship_att_control_usage}
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```
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airship_att_control <command> [arguments...]
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@@ -39,9 +37,7 @@ Source: [modules/control_allocator](https://github.com/PX4/PX4-Autopilot/tree/ma
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This implements control allocation. It takes torque and thrust setpoints
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as inputs and outputs actuator setpoint messages.
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<a id="control_allocator_usage"></a>
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### 用法
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### Usage {#control_allocator_usage}
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```
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control_allocator <command> [arguments...]
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@@ -53,7 +49,7 @@ control_allocator <command> [arguments...]
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status print status info
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```
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## fw_pos_control_l1
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## flight_mode_manager
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Source: [modules/flight_mode_manager](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/flight_mode_manager)
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@@ -62,9 +58,7 @@ Source: [modules/flight_mode_manager](https://github.com/PX4/PX4-Autopilot/tree/
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This implements the setpoint generation for all modes. It takes the current mode state of the vehicle as input
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and outputs setpoints for controllers.
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<a id="flight_mode_manager_usage"></a>
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### 用法
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### Usage {#flight_mode_manager_usage}
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```
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flight_mode_manager <command> [arguments...]
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@@ -76,7 +70,7 @@ flight_mode_manager <command> [arguments...]
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status print status info
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```
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## mc_att_control
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## fw_att_control
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Source: [modules/fw_att_control](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/fw_att_control)
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@@ -84,9 +78,7 @@ Source: [modules/fw_att_control](https://github.com/PX4/PX4-Autopilot/tree/main/
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fw_att_control is the fixed wing attitude controller.
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<a id="fw_att_control_usage"></a>
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### 用法
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### Usage {#fw_att_control_usage}
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```
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fw_att_control <command> [arguments...]
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@@ -107,9 +99,7 @@ Source: [modules/fw_pos_control](https://github.com/PX4/PX4-Autopilot/tree/main/
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fw_pos_control is the fixed-wing position controller.
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<a id="fw_pos_control_usage"></a>
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### 用法
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### Usage {#fw_pos_control_usage}
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```
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fw_pos_control <command> [arguments...]
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@@ -130,9 +120,7 @@ Source: [modules/fw_rate_control](https://github.com/PX4/PX4-Autopilot/tree/main
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fw_rate_control is the fixed-wing rate controller.
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<a id="fw_rate_control_usage"></a>
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### 用法
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### Usage {#fw_rate_control_usage}
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```
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fw_rate_control <command> [arguments...]
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@@ -156,13 +144,14 @@ setpoints (`vehicle_attitude_setpoint`) as inputs and outputs a rate setpoint.
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The controller has a P loop for angular error
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The different internal modes are implemented as separate classes that inherit from a common base class <code>NavigatorMode</code>. The member <code>_navigation_mode</code> contains the current active mode.
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Publication documenting the implemented Quaternion Attitude Control:
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Nonlinear Quadrocopter Attitude Control (2013)
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by Dario Brescianini, Markus Hehn and Raffaello D'Andrea
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Institute for Dynamic Systems and Control (IDSC), ETH Zurich
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https://www.research-collection.ethz.ch/bitstream/handle/20.500.11850/154099/eth-7387-01.pdf
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<a id="mc_att_control_usage"></a>
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### 用法
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### Usage {#mc_att_control_usage}
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```
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mc_att_control <command> [arguments...]
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@@ -175,7 +164,7 @@ mc_att_control <command> [arguments...]
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status print status info
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```
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## navigator
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## mc_pos_control
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Source: [modules/mc_pos_control](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/mc_pos_control)
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@@ -188,9 +177,7 @@ Output of the velocity controller is thrust vector that is split to thrust direc
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The controller doesn't use Euler angles for its work, they are generated only for more human-friendly control and
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logging.
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<a id="mc_pos_control_usage"></a>
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### 用法
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### Usage {#mc_pos_control_usage}
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```
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mc_pos_control <command> [arguments...]
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@@ -214,9 +201,7 @@ via `manual_control_setpoint` topic) as inputs and outputs actuator control mess
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The controller has a PID loop for angular rate error.
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<a id="mc_rate_control_usage"></a>
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### 用法
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### Usage {#mc_rate_control_usage}
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```
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mc_rate_control <command> [arguments...]
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@@ -247,9 +232,7 @@ The member `_navigation_mode` contains the current active mode.
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Navigator publishes position setpoint triplets (`position_setpoint_triplet_s`), which are then used by the position
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controller.
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<a id="navigator_usage"></a>
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### 用法
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### Usage {#navigator_usage}
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```
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navigator <command> [arguments...]
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@@ -273,9 +256,7 @@ Source: [modules/rover_ackermann](https://github.com/PX4/PX4-Autopilot/tree/main
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Rover ackermann module.
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<a id="rover_ackermann_usage"></a>
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### 用法
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### Usage {#rover_ackermann_usage}
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```
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rover_ackermann <command> [arguments...]
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@@ -295,9 +276,7 @@ Source: [modules/rover_differential](https://github.com/PX4/PX4-Autopilot/tree/m
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Rover differential module.
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<a id="rover_differential_usage"></a>
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### 用法
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### Usage {#rover_differential_usage}
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```
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rover_differential <command> [arguments...]
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@@ -317,9 +296,7 @@ Source: [modules/rover_mecanum](https://github.com/PX4/PX4-Autopilot/tree/main/s
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Rover mecanum module.
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<a id="rover_mecanum_usage"></a>
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### 用法
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### Usage {#rover_mecanum_usage}
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```
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rover_mecanum <command> [arguments...]
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@@ -359,9 +336,7 @@ rover_pos_control status
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rover_pos_control stop
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```
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<a id="rover_pos_control_usage"></a>
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### 用法
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### Usage {#rover_pos_control_usage}
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```
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rover_pos_control <command> [arguments...]
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@@ -384,9 +359,7 @@ It takes torque and thrust setpoints as inputs and outputs
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actuator setpoint messages.
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```
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<a id="spacecraft_usage"></a>
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### 用法
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### Usage {#spacecraft_usage}
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```
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spacecraft <command> [arguments...]
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@@ -425,9 +398,7 @@ uuv_att_control status
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uuv_att_control stop
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```
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<a id="uuv_att_control_usage"></a>
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### 用法
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### Usage {#uuv_att_control_usage}
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```
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uuv_att_control <command> [arguments...]
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@@ -465,9 +436,7 @@ uuv_pos_control status
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uuv_pos_control stop
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```
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<a id="uuv_pos_control_usage"></a>
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### 用法
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### Usage {#uuv_pos_control_usage}
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```
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uuv_pos_control <command> [arguments...]
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@@ -487,9 +456,7 @@ Source: [modules/vtol_att_control](https://github.com/PX4/PX4-Autopilot/tree/mai
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fw_att_control is the fixed wing attitude controller.
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<a id="vtol_att_control_usage"></a>
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### 用法
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### Usage {#vtol_att_control_usage}
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```
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vtol_att_control <command> [arguments...]
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