mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-22 00:28:30 -04:00
AP_Scripting: remove original aerobatics example to avoid confusion
This commit is contained in:
Henry Wurzburg
Andrew Tridgell
parent
fa81f7813c
commit
82235163a2
@ -1,395 +0,0 @@
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-- perform simple aerobatic manoeuvres in AUTO mode
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local running = false
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local roll_stage = 0
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local ROLL_TCONST = param:get('RLL2SRV_TCONST') * 0.5
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local PITCH_TCONST = param:get('PTCH2SRV_TCONST') * 0.5
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DO_JUMP = 177
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NAV_WAYPOINT = 16
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k_throttle = 70
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function bind_param(name)
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local p = Parameter()
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assert(p:init(name), string.format('could not find %s parameter', name))
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return p
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end
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local SCR_USER1 = bind_param("SCR_USER1") -- height P gain
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local SCR_USER2 = bind_param("SCR_USER2") -- height I gain
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local SCR_USER3 = bind_param("SCR_USER3") -- throttle FF from pitch
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local SCR_USER4 = bind_param("SCR_USER4") -- height knifeedge addition for pitch
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local SCR_USER5 = bind_param("SCR_USER5") -- speed P gain
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local SCR_USER6 = bind_param("SCR_USER6") -- speed I gain
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local TRIM_THROTTLE = bind_param("TRIM_THROTTLE")
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local TRIM_ARSPD_CM = bind_param("TRIM_ARSPD_CM")
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local last_roll_err = 0.0
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local last_id = 0
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local initial_yaw_deg = 0
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local wp_yaw_deg = 0
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local initial_height = 0
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-- constrain a value between limits
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function constrain(v, vmin, vmax)
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if v < vmin then
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v = vmin
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end
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if v > vmax then
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v = vmax
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end
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return v
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end
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-- a controller to target a zero roll angle, coping with inverted flight
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-- output is a body frame roll rate, with convergence over time tconst in seconds
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function roll_zero_controller(tconst)
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local roll_deg = math.deg(ahrs:get_roll())
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local pitch_deg = math.deg(ahrs:get_pitch())
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local roll_err = 0.0
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if math.abs(pitch_deg) > 85 then
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-- close to 90 we retain the last roll rate
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roll_err = last_roll_err
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elseif roll_deg > 90 then
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roll_err = 180 - roll_deg
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elseif roll_deg < -90 then
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roll_err = (-180) - roll_deg
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else
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roll_err = -roll_deg
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end
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last_roll_err = roll_err
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return roll_err / tconst
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end
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function wrap_360(angle)
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local res = math.fmod(angle, 360.0)
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if res < 0 then
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res = res + 360.0
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end
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return res
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end
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function wrap_180(angle)
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local res = wrap_360(angle)
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if res > 180 then
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res = res - 360
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end
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return res
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end
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-- a PI controller implemented as a Lua object
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local function PI_controller(kP,kI,iMax)
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-- the new instance. You can put public variables inside this self
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-- declaration if you want to
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local self = {}
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-- private fields as locals
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local _kP = kP or 0.0
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local _kI = kI or 0.0
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local _kD = kD or 0.0
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local _iMax = iMax
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local _last_t = nil
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local _I = 0
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local _P = 0
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local _total = 0
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local _counter = 0
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local _target = 0
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local _current = 0
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-- update the controller.
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function self.update(target, current)
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local now = millis():tofloat() * 0.001
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if not _last_t then
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_last_t = now
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end
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local dt = now - _last_t
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_last_t = now
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local err = target - current
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_counter = _counter + 1
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local P = _kP * err
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_I = _I + _kI * err * dt
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if _iMax then
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_I = constrain(_I, -_iMax, iMax)
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end
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local I = _I
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local ret = P + I
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_target = target
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_current = current
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_P = P
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_total = ret
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return ret
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end
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-- reset integrator to an initial value
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function self.reset(integrator)
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_I = integrator
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end
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function self.set_I(I)
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_kI = I
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end
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function self.set_P(P)
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_kP = P
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end
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function self.set_Imax(Imax)
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_iMax = Imax
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end
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-- log the controller internals
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function self.log(name, add_total)
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-- allow for an external addition to total
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logger.write(name,'Targ,Curr,P,I,Total,Add','ffffff',_target,_current,_P,_I,_total,add_total)
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end
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-- return the instance
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return self
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end
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local function height_controller(kP_param,kI_param,KnifeEdge_param,Imax)
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local self = {}
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local kP = kP_param
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local kI = kI_param
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local KnifeEdge = KnifeEdge_param
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local PI = PI_controller(kP:get(), kI:get(), Imax)
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function self.update(target)
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local target_pitch = PI.update(initial_height, ahrs:get_location():alt()*0.01)
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local roll_rad = ahrs:get_roll()
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local ke_add = math.abs(math.sin(roll_rad)) * KnifeEdge:get()
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target_pitch = target_pitch + ke_add
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PI.log("HPI", ke_add)
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return target_pitch
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end
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function self.reset()
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PI.reset(math.max(math.deg(ahrs:get_pitch()), 3.0))
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PI.set_P(kP:get())
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PI.set_I(kI:get())
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end
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return self
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end
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local height_PI = height_controller(SCR_USER1, SCR_USER2, SCR_USER4, 20.0)
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local speed_PI = PI_controller(SCR_USER5:get(), SCR_USER6:get(), 100.0)
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-- a controller to target a zero pitch angle and zero heading change, used in a roll
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-- output is a body frame pitch rate, with convergence over time tconst in seconds
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function pitch_controller(target_pitch_deg, target_yaw_deg, tconst)
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local roll_deg = math.deg(ahrs:get_roll())
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local pitch_deg = math.deg(ahrs:get_pitch())
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local yaw_deg = math.deg(ahrs:get_yaw())
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-- get earth frame pitch and yaw rates
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local ef_pitch_rate = (target_pitch_deg - pitch_deg) / tconst
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local ef_yaw_rate = wrap_180(target_yaw_deg - yaw_deg) / tconst
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local bf_pitch_rate = math.sin(math.rad(roll_deg)) * ef_yaw_rate + math.cos(math.rad(roll_deg)) * ef_pitch_rate
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local bf_yaw_rate = math.cos(math.rad(roll_deg)) * ef_yaw_rate - math.sin(math.rad(roll_deg)) * ef_pitch_rate
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return bf_pitch_rate, bf_yaw_rate
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end
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-- a controller for throttle to account for pitch
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function throttle_controller(tconst)
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local pitch_rad = ahrs:get_pitch()
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local thr_ff = SCR_USER3:get()
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local throttle = TRIM_THROTTLE:get() + math.sin(pitch_rad) * thr_ff
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return constrain(throttle, 0.0, 100.0)
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end
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function do_axial_roll(arg1, arg2)
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-- constant roll rate axial roll
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if not running then
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running = true
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roll_stage = 0
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height_PI.reset()
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gcs:send_text(0, string.format("Starting roll"))
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end
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local roll_rate = arg1
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local throttle = arg2
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local pitch_deg = math.deg(ahrs:get_pitch())
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local roll_deg = math.deg(ahrs:get_roll())
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if roll_stage == 0 then
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if roll_deg > 45 then
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roll_stage = 1
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end
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elseif roll_stage == 1 then
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if roll_deg > -5 and roll_deg < 5 then
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running = false
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-- we're done
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gcs:send_text(0, string.format("Finished roll r=%.1f p=%.1f", roll_deg, pitch_deg))
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vehicle:nav_script_time_done(last_id)
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roll_stage = 2
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return
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end
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end
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if roll_stage < 2 then
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target_pitch = height_PI.update(initial_height)
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pitch_rate, yaw_rate = pitch_controller(target_pitch, wp_yaw_deg, PITCH_TCONST)
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vehicle:set_target_throttle_rate_rpy(throttle, roll_rate, pitch_rate, yaw_rate)
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end
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end
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local loop_stage = 0
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function do_loop(arg1, arg2)
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-- do one loop with controllable pitch rate and throttle
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if not running then
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running = true
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loop_stage = 0
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gcs:send_text(0, string.format("Starting loop"))
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end
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local pitch_rate = arg1
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local throttle = throttle_controller()
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local pitch_deg = math.deg(ahrs:get_pitch())
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local roll_deg = math.deg(ahrs:get_roll())
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if loop_stage == 0 then
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if pitch_deg > 60 then
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loop_stage = 1
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end
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elseif loop_stage == 1 then
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if math.abs(roll_deg) < 90 and pitch_deg > -5 and pitch_deg < 5 then
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running = false
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-- we're done
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gcs:send_text(0, string.format("Finished loop p=%.1f", pitch_deg))
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vehicle:nav_script_time_done(last_id)
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loop_stage = 2
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return
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end
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end
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if loop_stage < 2 then
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local roll_rate = roll_zero_controller(ROLL_TCONST)
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vehicle:set_target_throttle_rate_rpy(throttle, roll_rate, pitch_rate, 0)
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end
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end
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local rolling_circle_stage = 0
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local rolling_circle_yaw = 0
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local rolling_circle_last_ms = 0
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function do_rolling_circle(arg1, arg2)
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-- constant roll rate circle roll
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if not running then
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running = true
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rolling_circle_stage = 0
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rolling_circle_yaw = 0
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rolling_circle_last_ms = millis()
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height_PI.reset()
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speed_PI.set_P(SCR_USER5:get())
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speed_PI.set_I(SCR_USER6:get())
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speed_PI.reset(math.max(SRV_Channels:get_output_scaled(k_throttle), TRIM_THROTTLE:get()))
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gcs:send_text(0, string.format("Starting rolling circle"))
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end
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local radius = arg1
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local num_rolls = arg2
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local pitch_deg = math.deg(ahrs:get_pitch())
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local roll_deg = math.deg(ahrs:get_roll())
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local yaw_deg = math.deg(ahrs:get_yaw())
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local gspeed = ahrs:groundspeed_vector():length()
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local circumference = math.abs(math.pi * 2.0 * radius)
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local circle_time = circumference / gspeed
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local yaw_rate_dps = 360.0 / circle_time
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local now_ms = millis()
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local dt = (now_ms - rolling_circle_last_ms):tofloat() * 0.001
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rolling_circle_last_ms = now_ms
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if radius < 0.0 then
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yaw_rate_dps = -yaw_rate_dps
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end
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local roll_rate = (360.0 * num_rolls) / circle_time
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rolling_circle_yaw = rolling_circle_yaw + yaw_rate_dps * dt
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if rolling_circle_stage == 0 then
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if math.abs(rolling_circle_yaw) > 10.0 then
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rolling_circle_stage = 1
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end
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elseif rolling_circle_stage == 1 then
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if math.abs(rolling_circle_yaw) >= 360.0 then
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running = false
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-- we're done
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gcs:send_text(0, string.format("Finished rollcircle r=%.1f p=%.1f", roll_deg, pitch_deg))
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vehicle:nav_script_time_done(last_id)
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rolling_circle_stage = 2
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return
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end
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end
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local target_roll = num_rolls * math.abs(rolling_circle_yaw)
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local roll_error = wrap_180(target_roll - roll_deg)
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local roll_error_P = 0.5
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local roll_rate_corrected = roll_rate + roll_error * roll_error_P
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if rolling_circle_stage < 2 then
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target_pitch = height_PI.update(initial_height)
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vel = ahrs:get_velocity_NED()
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throttle = speed_PI.update(TRIM_ARSPD_CM:get()*0.01, vel:length())
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throttle = constrain(throttle, 0, 100.0)
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speed_PI.log("SPI", 0.0)
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pitch_rate, yaw_rate = pitch_controller(target_pitch, wrap_360(rolling_circle_yaw+initial_yaw_deg), PITCH_TCONST)
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vehicle:set_target_throttle_rate_rpy(throttle, roll_rate_corrected, pitch_rate, yaw_rate)
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end
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end
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--- get a location object for a given WP number
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function get_wp_location(i)
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local m = mission:get_item(i)
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local loc = Location()
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loc:lat(m:x())
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loc:lng(m:y())
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loc:relative_alt(false)
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loc:terrain_alt(false)
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loc:origin_alt(false)
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loc:alt(math.floor(m:z()*100))
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return loc
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end
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function resolve_jump(i)
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local m = mission:get_item(i)
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while m:command() == DO_JUMP do
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i = math.floor(m:param1())
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m = mission:get_item(i)
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end
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return i
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end
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function update()
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id, cmd, arg1, arg2 = vehicle:nav_script_time()
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if id then
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if id ~= last_id then
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-- we've started a new command
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running = false
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last_id = id
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initial_yaw_deg = math.deg(ahrs:get_yaw())
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initial_height = ahrs:get_location():alt()*0.01
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-- work out yaw between previous WP and next WP
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local cnum = mission:get_current_nav_index()
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local loc_prev = get_wp_location(cnum-1)
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local loc_next = get_wp_location(resolve_jump(cnum+1))
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wp_yaw_deg = math.deg(loc_prev:get_bearing(loc_next))
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end
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if cmd == 1 then
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do_axial_roll(arg1, arg2)
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elseif cmd == 2 then
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do_loop(arg1, arg2)
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elseif cmd == 3 then
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do_rolling_circle(arg1, arg2)
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end
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else
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running = false
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end
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return update, 10
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end
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return update()
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