diff --git a/libraries/SITL/SIM_SingleCopter.cpp b/libraries/SITL/SIM_SingleCopter.cpp
new file mode 100644
index 0000000000..a0fefd38c5
--- /dev/null
+++ b/libraries/SITL/SIM_SingleCopter.cpp
@@ -0,0 +1,94 @@
+/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
+/*
+ This program is free software: you can redistribute it and/or modify
+ it under the terms of the GNU General Public License as published by
+ the Free Software Foundation, either version 3 of the License, or
+ (at your option) any later version.
+
+ This program is distributed in the hope that it will be useful,
+ but WITHOUT ANY WARRANTY; without even the implied warranty of
+ MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
+ GNU General Public License for more details.
+
+ You should have received a copy of the GNU General Public License
+ along with this program. If not, see .
+ */
+/*
+ singlecopter simulator class
+*/
+
+#include "SIM_SingleCopter.h"
+
+#include
+
+using namespace SITL;
+
+SingleCopter::SingleCopter(const char *home_str, const char *frame_str) :
+ Aircraft(home_str, frame_str)
+{
+ mass = 2.0f;
+
+ /*
+ scaling from motor power to Newtons. Allows the copter
+ to hover against gravity when the motor is at hover_throttle
+ */
+ thrust_scale = (mass * GRAVITY_MSS) / hover_throttle;
+ frame_height = 0.1;
+}
+
+/*
+ update the copter simulation by one time step
+ */
+void SingleCopter::update(const struct sitl_input &input)
+{
+ // get wind vector setup
+ update_wind(input);
+
+ float actuator[4];
+ for (uint8_t i=0; i<4; i++) {
+ actuator[i] = constrain_float((input.servos[i]-1500) / 500.0f, -1, 1);
+ }
+ float thrust = constrain_float((input.servos[4]-1000) / 1000.0f, 0, 1);
+ float yaw_thrust = (actuator[0] + actuator[1] + actuator[2] + actuator[3]) * 0.25f * thrust;
+ float roll_thrust = (actuator[0] - actuator[2]) * 0.5f * thrust;
+ float pitch_thrust = (actuator[1] - actuator[3]) * 0.5f * thrust;
+
+ float torque_effect_accel = thrust * rotor_rot_accel;
+
+ // rotational acceleration, in rad/s/s, in body frame
+ Vector3f rot_accel(roll_thrust * roll_rate_max,
+ pitch_thrust * pitch_rate_max,
+ yaw_thrust * yaw_rate_max + torque_effect_accel);
+
+ // rotational air resistance
+ rot_accel.x -= gyro.x * radians(5000.0) / terminal_rotation_rate;
+ rot_accel.y -= gyro.y * radians(5000.0) / terminal_rotation_rate;
+ rot_accel.z -= gyro.z * radians(400.0) / terminal_rotation_rate;
+
+ // air resistance
+ Vector3f air_resistance = -velocity_air_ef * (GRAVITY_MSS/terminal_velocity);
+
+ // scale thrust to newtons
+ thrust *= thrust_scale;
+
+ accel_body = Vector3f(0, 0, -thrust / mass);
+ accel_body += dcm * air_resistance;
+
+ bool was_on_ground = on_ground(position);
+
+ update_dynamics(rot_accel);
+
+ // constrain height to the ground
+ if (on_ground(position) && !was_on_ground) {
+ // zero roll/pitch, but keep yaw
+ float r, p, y;
+ dcm.to_euler(&r, &p, &y);
+ dcm.from_euler(0, 0, y);
+
+ position.z = -(ground_level + frame_height - home.alt*0.01f);
+ velocity_ef.zero();
+ }
+
+ // update lat/lon/altitude
+ update_position();
+}
diff --git a/libraries/SITL/SIM_SingleCopter.h b/libraries/SITL/SIM_SingleCopter.h
new file mode 100644
index 0000000000..6d6278c31d
--- /dev/null
+++ b/libraries/SITL/SIM_SingleCopter.h
@@ -0,0 +1,53 @@
+/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
+/*
+ This program is free software: you can redistribute it and/or modify
+ it under the terms of the GNU General Public License as published by
+ the Free Software Foundation, either version 3 of the License, or
+ (at your option) any later version.
+
+ This program is distributed in the hope that it will be useful,
+ but WITHOUT ANY WARRANTY; without even the implied warranty of
+ MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
+ GNU General Public License for more details.
+
+ You should have received a copy of the GNU General Public License
+ along with this program. If not, see .
+ */
+/*
+ single copter simulator class
+*/
+
+#pragma once
+
+#include "SIM_Aircraft.h"
+#include
+
+namespace SITL {
+
+/*
+ a single copter simulator
+ */
+class SingleCopter : public Aircraft {
+public:
+ SingleCopter(const char *home_str, const char *frame_str);
+
+ /* update model by one time step */
+ void update(const struct sitl_input &input);
+
+ /* static object creator */
+ static Aircraft *create(const char *home_str, const char *frame_str) {
+ return new SingleCopter(home_str, frame_str);
+ }
+
+private:
+ float terminal_rotation_rate = 4*radians(360.0f);
+ float hover_throttle = 0.65f;
+ float terminal_velocity = 40;
+ float rotor_rot_accel = radians(20) * AP_MOTORS_MATRIX_YAW_FACTOR_CW;
+ float roll_rate_max = radians(700);
+ float pitch_rate_max = radians(700);
+ float yaw_rate_max = radians(700);
+ float thrust_scale;
+};
+
+} // namespace SITL