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Ap_Scripting: fixed plane aerobatics for full yaw rate control

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Andrew Tridgell 2021-11-26 10:18:39 +11:00 committed by Peter Barker
parent 56870ad7d6
commit 3a3cb92efd
1 changed files with 4 additions and 19 deletions
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23
libraries/AP_Scripting/examples/plane_aerobatics.lua
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@ -18,14 +18,6 @@ assert(scr_user3_param:init('SCR_USER3'), 'could not find SCR_USER3 parameter')
local last_roll_err = 0.0
local last_id = 0
-- find our rudder channel
local RUDDER_CHAN = SRV_Channels:find_channel(21)
local RUDDER_TRIM = param:get("SERVO" .. RUDDER_CHAN + 1 .. "_TRIM")
local RUDDER_REVERSED = param:get("SERVO" .. RUDDER_CHAN + 1 .. "_REVERSED")
local RUDDER_MIN = param:get("SERVO" .. RUDDER_CHAN + 1 .. "_MIN")
local RUDDER_MAX = param:get("SERVO" .. RUDDER_CHAN + 1 .. "_MAX")
local RUDDER_THROW = (RUDDER_MAX - RUDDER_MIN) * 0.5
-- constrain a value between limits
function constrain(v, vmin, vmax)
if v < vmin then
@ -63,9 +55,8 @@ function pitch_controller(target_pitch_deg, tconst)
local roll_deg = math.deg(ahrs:get_roll())
local pitch_deg = math.deg(ahrs:get_pitch())
local pitch_rate = (target_pitch_deg - pitch_deg) * math.cos(math.rad(roll_deg)) / tconst
RUDDER_GAIN = scr_user1_param:get()
local rudder = pitch_deg * RUDDER_GAIN * math.sin(math.rad(roll_deg)) / tconst
return pitch_rate, rudder
local yaw_rate = -(target_pitch_deg - pitch_deg) * math.sin(math.rad(roll_deg)) / tconst
return pitch_rate, yaw_rate
end
-- a controller for throttle to account for pitch
@ -103,14 +94,8 @@ function do_axial_roll(arg1, arg2)
end
if roll_stage < 2 then
target_pitch = scr_user2_param:get()
pitch_rate, rudder = pitch_controller(target_pitch, PITCH_TCONST)
vehicle:set_target_throttle_rate_rpy(throttle, roll_rate, pitch_rate, 0)
if RUDDER_REVERSED == 1 then
rudder = -rudder
end
local rudder_out = math.floor(RUDDER_TRIM + RUDDER_THROW * rudder)
rudder_out = constrain(rudder_out, RUDDER_MIN, RUDDER_MAX)
SRV_Channels:set_output_pwm_chan_timeout(RUDDER_CHAN, rudder_out, 50)
pitch_rate, yaw_rate = pitch_controller(target_pitch, PITCH_TCONST)
vehicle:set_target_throttle_rate_rpy(throttle, roll_rate, pitch_rate, yaw_rate)
end
end