ardupilot/libraries/AP_Scripting/applets/VTOL-quicktune.lua

419 lines
11 KiB
Lua
Raw Normal View History

--[[
fast tuning of VTOL gains for multirotors and quadplanes
This should be used in QLOITER mode for quadplanes and LOITER mode
for copters, although it will work in other VTOL modes
--]]
local PARAM_TABLE_KEY = 8
local PARAM_TABLE_PREFIX = "QUIK_"
local is_quadplane = false
local atc_prefix = "ATC"
-- bind a parameter to a variable
function bind_param(name)
local p = Parameter()
assert(p:init(name), string.format('could not find %s parameter', name))
return p
end
-- add a parameter and bind it to a variable
function bind_add_param(name, idx, default_value)
assert(param:add_param(PARAM_TABLE_KEY, idx, name, default_value), string.format('could not add param %s', name))
return bind_param(PARAM_TABLE_PREFIX .. name)
end
-- setup quicktune specific parameters
assert(param:add_table(PARAM_TABLE_KEY, PARAM_TABLE_PREFIX, 7), 'could not add param table')
local QUIK_ENABLE = bind_add_param('ENABLE', 1, 0)
local QUIK_AXES = bind_add_param('AXES', 2, 7)
local QUIK_DOUBLE_TIME = bind_add_param('DOUBLE_TIME', 3, 10)
local QUIK_GAIN_MARGIN = bind_add_param('GAIN_MARGIN', 4, 70)
local QUIK_OSC_SMAX = bind_add_param('OSC_SMAX', 5, 5)
local QUIK_YAW_P_MAX = bind_add_param('YAW_P_MAX', 6, 0.5)
local QUIK_YAW_D_MAX = bind_add_param('YAW_D_MAX', 7, 0.01)
local INS_GYRO_FILTER = bind_param("INS_GYRO_FILTER")
local RCMAP_ROLL = bind_param("RCMAP_ROLL")
local RCMAP_PITCH = bind_param("RCMAP_PITCH")
local RCMAP_YAW = bind_param("RCMAP_YAW")
local RCIN_ROLL = rc:get_channel(RCMAP_ROLL:get())
local RCIN_PITCH = rc:get_channel(RCMAP_PITCH:get())
local RCIN_YAW = rc:get_channel(RCMAP_YAW:get())
local UPDATE_RATE_HZ = 40
local STAGE_DELAY = 4.0
local PILOT_INPUT_DELAY = 4.0
local YAW_FLTE_MAX = 2.0
local FLTD_MUL = 0.5
local FLTT_MUL = 0.5
-- SMAX to set if none set at start
local DEFAULT_SMAX = 50.0
-- work out vehicle type
if param:get("Q_A_RAT_RLL_SMAX") then
is_quadplane = true
atc_prefix = "Q_A"
gcs:send_text(0, "Quicktune for quadplane loaded")
elseif param:get("ATC_RAT_RLL_SMAX") then
is_quadplane = false
gcs:send_text(0, "Quicktune for multicopter loaded")
else
gcs:send_text(0, "Quicktune unknown vehicle")
return
end
-- get time in sections since boot
function get_time()
return millis():tofloat() * 0.001
end
local axis_names = { "RLL", "PIT", "YAW" }
local param_suffixes = { "FF", "P", "I", "D", "SMAX", "FLTT", "FLTD", "FLTE" }
local stages = { "D", "P" }
local stage = stages[1]
local last_stage_change = get_time()
local last_gain_report = get_time()
local last_pilot_input = get_time()
local slew_parm = nil
local slew_target = 0
local slew_delta = 0
local axes_done = {}
-- create params dictionary indexed by name, such as "RLL_P"
local params = {}
local param_saved = {}
local param_changed = {}
local need_restore = false
for i, axis in ipairs(axis_names) do
for j, suffix in ipairs(param_suffixes) do
local pname = axis .. "_" .. suffix
params[pname] = bind_param(atc_prefix .. "_" .. "RAT_" .. pname)
param_changed[pname] = false
end
end
-- reset to start
function reset_axes_done()
for i, axis in ipairs(axis_names) do
axes_done[axis] = false
end
stage = stages[1]
end
-- get all current param values into param_saved dictionary
function get_all_params()
for pname in pairs(params) do
param_saved[pname] = params[pname]:get()
end
end
-- restore all param values from param_saved dictionary
function restore_all_params()
for pname in pairs(params) do
local changed = param_changed[pname] and 1 or 0
if param_changed[pname] then
params[pname]:set(param_saved[pname])
param_changed[pname] = false
end
end
end
-- save all param values to storage
function save_all_params()
for pname in pairs(params) do
if param_changed[pname] then
params[pname]:set_and_save(params[pname]:get())
param_saved[pname] = params[pname]:get()
param_changed[pname] = false
end
end
end
-- setup a default SMAX if zero
function setup_SMAX()
for i, axis in ipairs(axis_names) do
local smax = axis .. "_SMAX"
if params[smax]:get() <= 0 then
adjust_gain(smax, DEFAULT_SMAX)
end
end
end
-- setup filter frequencies
function setup_filters()
for i, axis in ipairs(axis_names) do
local fltd = axis .. "_FLTD"
local fltt = axis .. "_FLTT"
local flte = axis .. "_FLTE"
adjust_gain(fltt, INS_GYRO_FILTER:get() * FLTT_MUL)
adjust_gain(fltd, INS_GYRO_FILTER:get() * FLTD_MUL)
if axis == "YAW" then
local FLTE = params[flte]
if FLTE:get() <= 0.0 or FLTE:get() > YAW_FLTE_MAX then
adjust_gain(flte, YAW_FLTE_MAX)
end
end
end
end
-- check for pilot input to pause tune
function have_pilot_input()
if (math.abs(RCIN_ROLL:norm_input_dz()) > 0 or
math.abs(RCIN_PITCH:norm_input_dz()) > 0 or
math.abs(RCIN_YAW:norm_input_dz()) > 0) then
return true
end
return false
end
reset_axes_done()
get_all_params()
-- 3 position switch
local quick_switch = nil
-- get the axis name we are working on, or nil for all done
function get_current_axis()
local axes = QUIK_AXES:get()
for i = 1, #axis_names do
local mask = (1 << (i-1))
local axis_name = axis_names[i]
if (mask & axes) ~= 0 and axes_done[axis_name] == false then
return axis_names[i]
end
end
return nil
end
-- get slew rate for an axis
function get_slew_rate(axis)
local roll_srate, pitch_srate, yaw_srate = AC_AttitudeControl:get_rpy_srate()
if axis == "RLL" then
return roll_srate
end
if axis == "PIT" then
return pitch_srate
end
if axis == "YAW" then
return yaw_srate
end
return 0.0
end
-- move to next stage of tune
function advance_stage(axis)
if stage == "D" then
stage = "P"
else
axes_done[axis] = true
stage = "D"
end
end
-- get param name, such as RLL_P, used as index into param dictionaries
function get_pname(axis, stage)
return axis .. "_" .. stage
end
-- change a gain
function adjust_gain(pname, value)
local P = params[pname]
need_restore = true
param_changed[pname] = true
P:set(value)
if string.sub(pname, -2) == "_P" then
-- also change I gain
local iname = string.gsub(pname, "_P", "_I")
local ffname = string.gsub(pname, "_P", "_FF")
local I = params[iname]
local FF = params[ffname]
if FF:get() > 0 then
-- if we have any FF on an axis then we don't couple I to P,
-- usually we want I = FF for a one sectond time constant for trim
return
end
param_changed[iname] = true
if string.sub(pname, 1, 3) == "YAW" then
-- for yaw, I is 1/10 of P
I:set(value*0.1)
else
-- otherwise I == P
I:set(value)
end
end
end
-- return gain multipler for one loop
function get_gain_mul()
return math.exp(math.log(2.0)/(UPDATE_RATE_HZ*QUIK_DOUBLE_TIME:get()))
end
function setup_slew_gain(pname, gain)
slew_parm = pname
slew_target = gain
slew_steps = UPDATE_RATE_HZ/2
slew_delta = (gain - params[pname]:get()) / slew_steps
end
function update_slew_gain()
if slew_parm ~= nil then
local P = params[slew_parm]
local axis = string.sub(slew_parm, 1, 3)
local ax_stage = string.sub(slew_parm, -1)
adjust_gain(slew_parm, P:get()+slew_delta)
slew_steps = slew_steps - 1
logger.write('QUIK','SRate,Gain,Param', 'ffn', get_slew_rate(axis), P:get(), axis .. ax_stage)
if slew_steps == 0 then
gcs:send_text(0, string.format("%s %.4f", slew_parm, P:get()))
slew_parm = nil
end
end
end
-- return gain limits on a parameter, or 0 for no limit
function gain_limit(pname)
if string.sub(pname, 1, 3) == "YAW" then
local suffix = string.sub(pname, -2)
if suffix == "_P" then
return QUIK_YAW_P_MAX:get()
end
if suffix == "_D" then
return QUIK_YAW_D_MAX:get()
end
end
return 0.0
end
function reached_limit(pname, gain)
local limit = gain_limit(pname)
if limit > 0.0 and gain >= limit then
return true
end
return false
end
-- main update function
function update()
if quick_switch == nil then
quick_switch = rc:find_channel_for_option(300)
end
if quick_switch == nil or QUIK_ENABLE:get() < 1 then
return
end
if have_pilot_input() then
last_pilot_input = get_time()
end
local sw_pos = quick_switch:get_aux_switch_pos()
if sw_pos == 0 or not arming:is_armed() or not vehicle:get_likely_flying() then
-- abort, revert parameters
if need_restore then
need_restore = false
restore_all_params()
gcs:send_text(0, string.format("Tuning: reverted"))
end
reset_axes_done()
return
end
if sw_pos == 2 then
-- save all params
if need_restore then
need_restore = false
save_all_params()
gcs:send_text(0, string.format("Tuning: saved"))
end
end
if sw_pos ~= 1 then
return
end
if get_time() - last_stage_change < STAGE_DELAY then
update_slew_gain()
return
end
axis = get_current_axis()
if axis == nil then
-- nothing left to do
return
end
if not need_restore then
-- we are just starting tuning, get current values
gcs:send_text(0, string.format("Tuning: starting tune"))
get_all_params()
setup_SMAX()
setup_filters()
end
if get_time() - last_pilot_input < PILOT_INPUT_DELAY then
return
end
local srate = get_slew_rate(axis)
local pname = get_pname(axis, stage)
local P = params[pname]
local oscillating = srate > QUIK_OSC_SMAX:get()
local limited = reached_limit(pname, P:get())
if limited or oscillating then
local reduction = (100.0-QUIK_GAIN_MARGIN:get())*0.01
if not oscillating then
reduction = 1.0
end
local new_gain = P:get() * reduction
local limit = gain_limit(pname)
if limit > 0.0 and new_gain > limit then
new_gain = limit
end
setup_slew_gain(pname, new_gain)
logger.write('QUIK','SRate,Gain,Param', 'ffn', srate, P:get(), axis .. stage)
gcs:send_text(0, string.format("Tuning: %s done", pname))
advance_stage(axis)
last_stage_change = get_time()
if get_current_axis() == nil then
gcs:send_text(0, string.format("Tuning: DONE"))
end
else
local new_gain = P:get()*get_gain_mul()
if new_gain <= 0.0001 then
new_gain = 0.001
end
adjust_gain(pname, new_gain)
logger.write('QUIK','SRate,Gain,Param', 'ffn', srate, P:get(), axis .. stage)
if get_time() - last_gain_report > 3 then
last_gain_report = get_time()
gcs:send_text(0, string.format("%s %.4f sr:%.2f", pname, new_gain, srate))
end
end
end
-- wrapper around update(). This calls update() at 10Hz,
-- and if update faults then an error is displayed, but the script is not
-- stopped
function protected_wrapper()
local success, err = pcall(update)
if not success then
gcs:send_text(0, "Internal Error: " .. err)
-- when we fault we run the update function again after 1s, slowing it
-- down a bit so we don't flood the console with errors
--return protected_wrapper, 1000
return
end
return protected_wrapper, 1000/UPDATE_RATE_HZ
end
-- start running update loop
return protected_wrapper()