FlightGear - Flight Simulator FGAddon

Junkers W 34: Complete revision of the FDM. Added Bumpmap. Reorganization of files. Add freight as an option

Junkers W 34: Complete revision of the FDM. Added Bumpmap. Reorganization of files. Add freight as an option

Junkers W 34: Complete revision of the FDM. Added Bumpmap. Reorganization of files. Add freight as an option

SpaceShuttle milestone 13

Changes
-------------------------------------------------
Launch site location check before Lift Off (Wrong or Correct Location
help messages 15s after sim unpaused)

TAEM low energy fault messages inhibited when Shuttle is on the 747

Interrupt function for running/hanging Lambert targeting

Unhide panel O8 covers

Black bg for MDU dialogs

Activate NH3 boiler when starting the gliding test on carrier aircraft

Fix missing resume to VERT SIT in MM 603

Burn acceleration as a function of weight/burn mode in the
set_acceleration nasal function

Spurious LH2/LO2 alarm due to high lateral acceleration during first
roll after lift off fixed

Early 2EO Blue management if abort activated during stage 1

Bucket messages disabled in case of engine failure(s)

Fix typo for entry channel activation during OPS 6 (relative velocity
function needed)

Make DPS parser fail rather than PFD loop when no valid auto sequence
is entered in PDRS CONTROL, define first auto sequenace as number 1 in
display whereas internally the array index is 0

Set attach roll to 180 for HST

Orient hst.ac along the grapple target and add rotation offsets in
payload bay

Higher G for Nz Activation // Entry max hdot targeted tunning

TAEM transition for OPS 6 fix: No transition if alpha recovery or nz
hold phases are active

2EO pitch bias ( minimum 50° before SRB Sep)

Panel 08 Forward RCS switch animation

Panel 08 FWD RCS talkback animation and switch separation

Change offside distance of RMS camera from 30cm to 20cm

Add missing texture for HST

Revert "Change RMS arm wrist roll and HST target orientation"

This reverts commit 47d3ab1cd9cd441e0c9061ab22e9f3a687dcbd86.

Hdot ref fine tunning for entry traj5 / Execute condition for channels
to not be runned elsewhere than in Entry/TAEM

Energy ladder clamp values fine tunning

Fix another typo in save

Typo correction

Change RMS arm wrist roll and HST target orientation

More entry state saved properties

More valves to saved state

Start on RCS valve config save

Yet more switch positions to saved state

2eo Green / SE OPS 3 boundary fix for redesignation value

Abort boundaries logic in Nasal and jsbsim channel with conditionnal
to be runned one time only

Reverse sign for ADI Rate as per OI-33 (end of SCOM)

Another level for MDU update speed / Abort Boundary Update function

Polar Mission and high altitude insertion from Vandenberg

Fix droop guidance engage bug and TAL MECO targeting for low Mach
numbers

De-activate position recording in glide loop

SM ( PASS in OPS 2 or BFS elsewhere) dependency check for fault
messages / Backup C/W triggering

Reset trajectory history on state resume

Fix bugs on trajectory display

Fix payload attachment point to nodepad function

Nz target magenta line on Accel Arc for Nz Hold // CA appendix

2EO Green / Droop Inertial speed boundary takes into account TAL
redesignation single engine ops 3 new Vi boundary

No PEG4/7 values reset between MM transition

Fix: MPS LH2/LO2 alarm will not trigger anymore shortly after liftoff
(BFS)

Payload writes attachment point to notepad

Re-tuned low energy entry scenario

Add fuel cell efficiency to saved state

Help-class voice reminder to remember ammonia boilers at TAEM
interface

Grapple target

Abort Boundaries Voice Callouts

2 EO Blue/Green and 2 EO Green/Single Engine OPS 3 boundaries as a
function of Launch Inclination

2EO green yaw steering ending trigger (hdot and KEAS)

Correct yaw steering (left) for Bermuda Opportuniy 2 EO Green

GPC failure fault messages / F7 Yellow Light "GPC"

Square Brackets in SSU font mod / setFont erased from relevant dps
files

Tentative fix for the NO Y JET mode - parameters might still be
optimized

Add SRMS view offside the end effector

Stage 1 Open Loop Guidance based on JSB sim tables instead of Nasal
conditionnals // Load relief protection

Typo fix for MPS helium pressure fault messages

Bug fix: Delta Az white box recalled if TAEM transition happens during
a roll reversal

Alpha nominal ladder marker better property

Guidance box square and trailers logic for entry display

Time to HAC ladder/marker depending on HAC turn left or right

Delta Az fix for TAEM guidance

More Delta Az angle fixing

Save also ADI ref, CRT-IDP settings and TVC valve status

PD-controller for freon loop, is a lot more stable, but still trips
freon alarm once due to initial transits

Add engine controller and helium switches to saved state

Tentative fix for Delta Az issue for due north groundtrack

Payload bay manager checks for over-occupancy

Add manual MECO check via cutoff buttons to TAL MECO condition

OMS2 auto loaded PEG4 circularisation burn or PEG 7 Phasing burn //
Launch Window Rinc 0.05°

Daz/GS out of limits blinking markers // Medium Rate TAEM Xrange HAC
// Ascent ADI Pitch error flipped if RTHU occured

Fix: Velocity Cutoff ladder activated close to MECO to avoid marker
movement when close to PPA ( high Vrel)

Include SERC into forced control mode transition

Fix BFS->PASS transition in simplified DPS mode, this should just work

S-turns ending condition ( actual E/W below nominal E/W + 10000 ft)

OPS6 Transition at 100 Nm // RCS yaw deactivation in glide loop for
RTLS

PEG 4 iterations up to 50 (like for Lambert)

Auto OMS 2 function // Trim auto load added // OMS2 loaded at mm105
transition

Fix Spaghetti display when mm 304 cycled with PRO/EXE

i loaded OMS1/2 autoload for ISS and earlysts mission file

Switch SERC on only if one and only one engine is available, no SERC
for three engines off

Require approximate attitude agreement when grabbing a payload from
the payload bay

We probably shouldn't force the number of engines to 1 when checking
contingency abort...

Terminate regular auto launch guidance when RTLS is declared

Typo fix for Speedbrakes mode item 39

Preparation Work for Wp1 computation in mm 304 // Hac radius Wp1 fixed
// SB logic below 3kft

RTLS handover below 110Nm // TAEM nominal data up to 120kfeet for
GRTLS

Drag error tunning / Speedbrakes functions tunning / GRTLS Energy over
Weight functions extended up to 110Nm

Use all cutoff buttons depressed as valid MECO signal

Grab check for free-floating HST

Obsolete stand-alone HST management class, use instead an instance of
the payload class

Give HST 120 seconds deployment time

Deployment trigger for released payloads

All caps spelling for HST in mission file

Mission files can write notepad entries

MCC answers are recorded in notepad

Scenario can write notepad lines, revised de-orbit scenario

Notepad dialog

Viable de-orbit scenario, needs some tuning

Trigger SSME REPOSITION failure search only in MM304

Include TVC isolation valve opening into de-orbit preparation
checklist to avoid SSME repos error

Let the scenario format accept a pre-loaded burn plan

Veto APU underspeed check also when starting from the GUI

Suppress APU underspeed error during startup, reverse throttle
animation

Change targeted REI in MCC routine - needs to be tested

Reformulate nested conditionals in switch statements

Trailer update speed fix

Fix path to sound file

Typo fixes

Speedbrakes earlier activation for Energy modulation/ narrower
deadband +/- 4000 feet E/W

Suppress hydraulic system lowpressure error when initializing on-orbit

TAEM AP qbar max protection (300 psf above mach 1/ 350 psf below mach
1)

REI 4200 Nm instead of 3800 Nm

Earlier activation of entry drag deviation function (2700 Nm)

More accurate coordinates for Edwards Entry target

Stronger pull up // TAEM target recalculation for better accuracy //
No Sturn for HAC > 200°

Spec 50 item 41 leads to Entry computation (304)/TAEM computation(305)

Hac radius deviation X-range // Blinking Loc/GS/Time marker

New picture for lakebed landing scenario

Alpha modulation previous value // need to be fine tunned for new
guidance

Rudder active original value to avoid loss of control at fdm
transition

Altitude QFE for Glidepath calculations // Pull up logic to enter the
HAC below Mach 1

Radius factor for HAC size takes into account MEP or NEP

No Yaw Jet former Vspeed target function // Hac radius factor as a
function of altitude agl and MEP/NEP point

Actual Alpha marker will blink if different from nominal one ( > 2°)

Edwards Lakebed 23 (STS1) added for TAEM only

Selection of Item 41 airfield triggers TAEM calculations // avoid to
be stuck if we cycle through it to the previous TAEM target

Altitude QFE for TAEM when TAEM guidance available

Revised high-E entry scenario, added entry to White Sands

Minor corrections to TAEM glidepath below 6 Nm (A/L)

Better logic for Spiral HAC // Distance takes into account in hac
radial error and hac radius shrinking

Adjust standard entry scenario to improved FDM

Trailer update speed goes from 29 seconds to 15s below 14 kft/s

Nominal entry Alpha small adjustement

Attitude errors for TAL pfd and OPS 1 BFS

Eileen stationkeeping precision - still need to tune parameters...

Use fcs/throttle-cmd-norm for SB/throttle, damage-heavy.wav for gear
break

New damage sounds

Suppress BFC warning on transition when no BFS computer is running

Typo fixes

RTLS bodyflap for GRTLS before TAEM

Scenarios update for new FDM, TAEM handover OPS3/6, Speedbrakes and
Bodyflap sensitivity

Entry guidance improvements: Roll Reversal Daz limits / Bodyflap logic

TAEM guidance improvement: HAC shrink/ E/W management / Speedbrakes
logic / Spec 50 scale

Entry/TAEM trajectory re-scaled and Nominal path values updated for
new FDM

Entry and TAEM guidance update

Fault messages for TAEM Low Energy // High G

DPS rework OPS 3

Remove placeholder CWS switch from options GUI dialog

Functions requiring new FDM activated

FDM improvements for Basic/Gear/Speedbrakes Cd/Cl, Bodyflap Cm

TAEM dps assets

Remove fuel dump key bindings, add key binding for end effector
grab/release command

Friction dependant scrape sound change

Adjust fuselage dynamic and static friction factors, sound for belly
landing

Activate throttle control on 602 transition to allow manual SB via
throttle lever

Correct SSME position and NH3 boiler on for TAEM/Approach scenarios

Inactivate some functions that require new FDM to avoid FG crash

Rate error for OPS6 // TAEM Medium rate logic // Max LD and AOA Green
Band indications

Speedbrake pushbutton toggle autothrottle on off in (systems/ap/)

Functions for entry/TAEM AP guidance

ISS launch window (Rinc 0.05°) and RTHU activated

RTHU tighter roll limit to avoid jittering

Get rid of faulty CWS alarm - nested tests seem to be the issue -
backward compatibility problem?

Invert throttle/SB mapping, get rid of old-style manual SB

Replace != by NE in conditionals

Allow throttle to control manual SB, to do that enable engine 1
throttle when transiting to OPS 304 or 602

Divorce AP throttle properties from manual throttle properties

Make remaining throttling commands as well as ignition command use the
SSME array interface

Clean unused old-style throttle commands already commented out

More orange in chute

Reduce parachutes transperancy

Add texture to chutes

TAL Meco speed target for new L/D

Arrow Marker left for Entry display

Hot Freon warning trigger OPS 1/6 (ascent)

Entry roll compensation veto typo correction

Body Flap correct angle values

Tentative save of IMU drift state

Orbit pfd fixes / Deeper Error and Rate Needles logic / Glideslope fix

Glideslope scale Spec 50

Add sense switch position and status to saved state

Item 22 cancelled no PEG 7 reset // NaN bug fixed

DPS pages typo fixes

Spec 34 PEG 7 logic when converged

SM displays rework

Water/Freon loop minor fine tunning for better fault management

Caution Warning System message faults extension (
Hyd/APU/ECLSS/FC/Heaters)

SM Sys sum up 1 and 2 rework

Typo fix

Specific font for Square bracket

Global nasal variables for peg4/7 MNVR display

Square brackets font typo mistake (.tff instead of .ttf)

R1 elec panel spring loaded switches and AC controllers//sensors logic

System Management realism setting

Previous merge (02/11/2020) minor corrections

Typos in effects file, wrong name defined in effect file

Fix tire textures

Blinking Scratchpad if not executed with a Terminator // Correction
for Dual Scratchpad/fault line blinking

BFS GNC overhaul display

OPS 2 GNC display overhaul ( plus SM 201//202 only)

OPS 0 PASS display overhaul

OPS 1/6 GNC dps overhaul ( including pfd.svg )

Blinking scratchpad if not executed with a correct terminator

SSME correct stowed position for OPS 2 // MPS/TVC valve dependant for
OPS1/3/6

Ascent/RTLS/MNVR display rework preparation

Minor corrections from previous merge (typo errors mainly)

C/W and fault logic/phraseology reworking

Font resizing ( width 680)

Nz-hold-tgt switch removed // Always Nz tgt from RTLS calculation

MEDS menu typo error

Enhanced Menu Items ( 2 Rows) and Red cross for poll fail

Adjustement for RTLS Nz Hold default value and switch trigger
parameter

MEDS Retexturing for APU/HYD, OMS/MPS, SPI , Maintenance Displays

HUD Resizing and font adjustement

Bolder Font SSU A

Animate Panel A12 misc heater switches

Automatically deploy HST solar panels using
systems/rendezvous/target/distance-m

Aaverage CWS background texture

Alpha tape ladder correction

Extensive rework of PFD for PASS display

Font properties

Font logic and color adjustments

Payload weight decreased

Read me erased

SSU Fonts adjusted for correct Greek letters Unicode Read Me to
copy/paste the fonts in FgRoot/fonts required for some pfd elements

Original stage 4 beta target function values

3 G's minimum throttle

Management of Inc-acquire-sign with East(West)wards Course Better
insertion accuracy 3G's minimum throttle in case of negative value

Decreasing in Inclination error Stage 4 starts earlier ( Vi= 16000
ft/s)

Correct HST Inclination and Launch Window

Reposition HST secured model

Rework of AutoLaunch.nas

Stage 1 Open Loop closer to real datas ( good margin at Max Q) Lofted
traj in case of early engine failure for later RTLS to come MECO
altitude around 350 kfeet ( adjustable with traj loft and mps bias
angle in mission.xml) Flight path angle target at MECO ( initial value
in mission.xml of 0.5° , ie. 200 ft/s of vertical speed ish at MECO)
Smoother thrust reduction when reaching 3G's Nx acceleration
Adjustements for new SSME performances TAL MECO around 360 kfeet with
a slight upward inertial flight path

Hdot PID adjustment

Typo mistake

Quality of life adjustments

Deadband less tight for MM104 through 106 ( before DAP config in OPS2)
Bucket Nominal thrust ( 104.5%) Several mission files preset (
Standard insertion early STS style/ ISS /HST )

For HST, Targeted Inc is at 35° to avoid sensibility in Inc targeting
near max inclination and 90 ° Launch Azimuth Datas for a full
eastward insertion are available in Green, top of hst.xml

Minor Adjustments

Minor Adjustements

Complete Rework of RTLS display, matching better new perfo and 1
engine out at Lift off lofted trajectory

Hardcoded staged 1/2 new trajectory ( so far, it was in mission.xml
overlay, still present in "false" for easy custome tunning)

Gamma Target at MECO added

Boundary Between 2EO Green and Single Engine OPS 109 Adjusted

Adjustment for Second Stage Display ( Centered trajectory )

Reorder rotations to RYP in TDRS payload animation

Reorder rotations to RYP in SPARTAN payload animation

Reorder rotations to RYP in HST payload animation

Tank Adjustments

Proper 2 Tank logic ( Fuel and Oxydizer) for External Tank Tank 0 and
3 are concerned

Minor Adjustement

Correct Order for item 4 (109%) and 50 ( 106%) in Spec 51 display

Minor Adjustments

New switch logic to avoid over pitch with Hdot guidance active. Based
on Guidance mode, engine remainings and Inertial speed.

Hdot PID tunning

Minor Adjustments

SRB separation at lower propellant remaining ( Sep at 2mn04 ish)
Minimum thrust for lift off adjusted ( SL 100% = 380000 lbs)

Minor adjustement

ET content based on new tank logic

SSME improvements

Slightly adjusted Nozzle area for correct Sea Level Thrust

SSME performance improvements

Oxi/Fuel logic Mixture ratio (6.25) Fuel Flow for 100 % // 470000 lbs
thrust

Change HST attachement point

Unpaired comment tag, add sum-wrist-yaw-deg and ang-wrist-roll-deg

Add flag to show solar cells on payload release

More HST payload adjustments, rotations, translation

HST payload tuning

Adjust HST payload positions, more configuration

More HST position adjustments

HST position and hook adjustments, new hook model

Reposition HST, new connection point

R2 Engine power switches re-texture, shape and color

Start of new HST payload

Add separated white ET model, xml and conditioned control

CO marker for TAL

Fix a couple of trajectory map issues

Inprove TAL trajectory handling

Handle SRB-sep during a stage 1 3EO

Shuttle-side fix for a weird JSBSim issue that was introduced in
2019.2 and may prevent brakes from working

Fix MET computation prior to liftoff

Training manager difficulty hard

Additions to failure training dialog

Start on random fault training scenario framework

GPC sync failure during ascent causes yellow engine status light
illumination

ET separation mode switch dilemma

Proper simulation of redline condition and limits shutdown inhibit

Cutoff button dilemma and failure, improve BFS SYS SUMM 1 display of
Helium data

Add isolatable leakage points, show He leaks on BFS SYS SUMM

Correct annunciation and consequences of data and command path
failures

Enable BFS-specific fault messaging, add Helium fault messages

Start on MPS command path failure

Simulate interconnect dynamics of leakage

Extend leakage manager to MPS helium

Helium drain rates of MPS seem to be lower than assumed, in particular
the pneumatic system should hardly use any helium during ascent

BF indicates MPS dump, preparation for He system leakage flows

Animate and activate helium interconnect switches on panel R2

Request for interconnect switches

MPS helium flow rework

Helium interconnect valves, first version

Fix typo in TAL scenario

Aichi M6A (Seiran): Reorganization of files. Procedural lights. Relative paths. Armament system (bomb and machine gun), complete folding of the aircraft. Revision of the FDM

Aichi M6A (Seiran): Reorganization of files. Procedural lights. Relative paths. Armament system (bomb and machine gun), complete folding of the aircraft. Revision of the FDM

Boeing PT 17 "Stearman" : Revision of the FDM. Procedural lights. Relative paths

Boeing PT 17 "Stearman" : Revision of the FDM. Procedural lights. Relative paths

Stampe SV 4: Revision of the FDM. Procedural lights. Relative paths

Stampe SV 4: Revision of the FDM. Procedural lights. Relative paths