SpaceShuttle Miletone 14
Changelog:
7317a2de Merge /u/dirteat/fgspaceshuttledev/ branch minver into development
f9c1c571 Set a (soft) minimal fg version to 2024.1
1c5e9b48 Initialize object before setting up the listener
cc71908d TAL MECO condition updated for new TAL PEG guidance
f680bf9c Ascent pfd improved for nominal ascent (crosstrack / inertial bearing) Improved for TAL (crosstrack / delta crosstrack / heading to max crosstrack circle) HSI pinned to 0 (insertion plan)
89aff76c Print functions deactivated
2b09edde ECEF to ECI at a given time frame converter
69634e65 TAL PEG guidance improved (MECO speed and crossrange computations)
a0f8cdee TAL initial alpha commanded (43°) fix for low speed MECO TAL(below 20000 ft/s)
f02a2ea1 Merge /u/dirteat/fgspaceshuttledev/ branch svg into development
91a8613a Merge /u/dirteat/fgspaceshuttledev/ branch timedisplay into development
b4a06f11 Save time-display-flag to ensure the wanted PDF timer display on resume
e83a015e Prevent Nasal error when errors grow too large near final
06e222fe Fix corrupted coordinates and svgparser errors
d1ec0dd4 New max residual for TACAN range (2Nm), Bearing (3°) and Probe Altitude (3000 ft) for Ratio computation
2544bcc3 Item 5 thrust vector roll tunable in OPS 202
25a9a76a Hotfix for automatic transition between mm602 and mm603 during RTLS
b5a0a334 Better transition between GRTLS and TAEM pitch wise (reset of Nz commanded)
7b48aa94 Fix for droop guidance that was bypassed during Intact Abort / Droop PEG target computed after droop guidance disengaged for better PEG reconvergence
b90c21e3 Add flame effects to SRB static model for MP visibility (conditionals on srb sep added)
b29a1ad7 Clean and fix mp aliasing for the local and remote models
5a80a4f7 Fix shader errors due to missing shadows on MP
5a9d382d Fix effects path for MP
1e49d450 Elevator command gain reverted to previous logic (no velocity dependency)
af2c3894 During Contigency abort with no ECAL, no automatic transition to TAEM at Mach 3.2 / OPS 603 needed
1649e8a5 Function to compute energy state and distance to alternate landing sites for Spec 54 / Nz Prebank deactivated / Acquisition turn tuned for higher bank during ECAL
974be7fb Delta azimuth in pfd is always positive
bc966528 Spec 54 Bearing dps extended to ECAL / Delta azimuth function
52a93616 Contigency Nz hold fine tunning for SMNZ coeff and max G's allowed for NZC (3 iso 2) Better transition for ibank (roll command at the end of Nz hold phase)
9069ecbc Bda scenario without preprogrammed failure
8493ab59 GRTLS guidance / 2EO Contigency Blue and Green / ECAL BDA guidance
c04b10b9 New ecal landing sites and Ivalo
aa3e6034 Autopilot and fcs improved for GRTLS new guidance
0be9a751 DPS and displays upgraded for the ecal/bda logic 1EO droop inh/ena ECAL/BDA inh/ena Energy management in mm602
a8301804 New mission files for ECAL and BDA test
976d1f8a cockpit: Make event timer switches spring loaded
1569be76 timer: Fix event timer drift
f4f1b81e Transition DAP fine tunning
8532f719 No Nz target limit for RTLS to avoid loss of control during transition phase
a25ae7d4 Hao (Franch Polynesia) ELS site landing site added (Item 40) / Mission file with TAL test from Vandenberg
4c295aaf Timer change for runway elevation computation / avoid a nil error in some case
7c813b06 Re-commit MP effect additions
9904533c Merge branch 'development' of ssh://wlbragg@.../p/fgspaceshuttledev/code into development
97c62ed1 MP additions, legacy MP code cleanup (leading /)
4fcd0543 More fixes to MNVR DPS page based on DPS documentation Arrow logic for OMS and Gimbal failures
387c11ef Auto/CSS logic during Ascent // Pushbutton lights off when not in Ascent/Entry phase
78813e1d SERC typo (yellow overbright when ON)
f0485d1e RTLS Nz hold phase 2.2G's max
f6fa1511 More work on MNVR dps page: OMS failure indicators, load cancel logic.
991040db Emergency chute deployement if SSME nozzles are not stowed correctly
f4f71ac4 MNVR dps page improvement for PEG7 input after guidance is loaded (cancel it)
9fb325ee Fix for spurious engine failure alarm after MECO
1b55d2ed External hd texture in dds instead of png (faster loading time)
db7e9797 HD livery, texture mapping and effect application corrections, gear bay thermal protection
febf8488 Add hidef texture tolivery system
d0414299 Instantaneous impact point function for spec 54
a2ce1d3d Spec 54 Entry Bearing new DPS display for entry
df39eff7 Transition between HAC and Prefinal fine tunned
cd7caad0 HD external texture
578ba512 Better transition between TAEM ACQ and HAC phase Proper function for time to HAC computation (displayed on pfd and Spec 50)
6d977394 Mission files updated for auto OMS burn load / Auto countdown. Parameters specified at the top of each mission files in Green
68088601 Fix race conditions in providing proximity coordinates
2fcafec5 Fix uninitialized values of payload pointer preventing the manager to provide proximity coordinates
87a3462f Fix typo in comment
0a7e4305 Fix multiple restarts of the proximity manager once a targets enter the proximity zone
261f1bea Bank sum error nulled before each iteration for HUD roll guidance (fix)
ff02f26e Merge /u/dirteat/fgspaceshuttledev/ branch develnext into development
442906a6 HUD roll flight director smoother logic for TAEM
17f22c19 Adding shadows' shaders required for 2020.4 in spare effect files
d3174b2e More accurate parameters for ISS launch window (RINC 0.05°) / 2mn countdown
014b1a79 Roll guidance logic for HUD flight director
3790aff7 TAEM AP roll channel based on roll rate commanded / Attitude error and HUD guidance adjusted
056c81c6 Remove lightmap shadows from CWS display
12c4d33e Correct parameter for Hud Velocity Vector and PFD pitch attidude error during TAEM (Nz commanded insted of H dot)
c32eae1e New MECO condition in case advanced MECO parameters are used
c1b26bed Inactivated logic for Low Energy Logic WIP
86d27cb0 Cutoff Velocity ladder adjusted for TAL target (MECO Vi = 23700 fts)
ca5af909 New mission file / STS1 and peg test file with SCOM part 9 parameters
7e6dc954 Advanced meco parameters Logic // It allows the user to enter proper PEG MECO parameter in mission file instead of targeted Apogee(MECO height, gamma, inertial velocity)
1a8faec8 TAL and droop PEG meco parameters fine tunned
99486830 TAL cutoff velocity ladder adjustement (MECO between Mach 24 and 25) and low propellant meco condition (meco when prop is under 0.5%)
5f980edb Bug fixes and better convergence test for time to go PEG criterion
69bae9f4 Older PEG file removed
2ef9c8ee More stable jsbsim parameter for Nx computation and limits (better 3Gs throttling)
20c81e48 Main dev repo shuttle.xml version 22_02_2022
5e394320 Merge branch on the forl with main dev branch 21_02_2022
423acb8c Add a slider in rms operation to control CCTV overlay brightness
35455d3a Add listener on rms power to create and destroy CCTV canvas
92618235 Add cctv.nas module for the rms CCTV overlay canvas
ec11fc75 No RTHU for PEG test (more stable)
ed6b6cf1 Unified Powered Flight Guidance first implementation / Used for Nominal /TAL /ATO guidance
44856c2c Rodrigues Euler rotation formula for PEG intial guess
55b22e8b Debug isnan added to avoid NaN error for Normalization
87a4481e New PFD elements from Power Explicit Guidance: Fine count for MECO / Attitude error needles logic for PEG convergence / Dynamic MECO velocity cue
09e69c9b New option for Direct/Standard Insertion in the Auto Launch Dialog menu
bb9f1231 Merge branch 'development' into cleaneffect
effbb7d2 Power Expicit Guidance for Ascent core code finished / test phase / no output to jsbsim guidance yet
aaf7ceda Print functions deactivated / Older jsbsim functions used for previous Entry Guidance deactivated
5843e722 3d matrix product and a fix to avoid NaN with vector normalization by 0
8f477f7e Final HAC radius shrinking logic in case of Low Energy Condition during HAC
cb33b89a Roll error based on Entry guidance global variable
d31377be Fix paths to use only effects from PayloadBay/HST
2ae54a0c Rename supposedly unused old HST directory
ecf7fd65 Initial work on Power Explicit Guidance (WIP) and Conic State Extrapolation Routine (finished)
177ec252 TAL alpha logic before first pullout (43° to avoid to high temperatures)
21890f33 Stronger condition for TAEM computation (305/603) to avoid breakage during TAL abort
c1f727be Hdot ref for 305 display coming from Entry workbook hdot scale height formula
84d10b5d New entry code: Entry guidance finished // first step of autopilot output filtered to jsbsim (Deadband, etc) // Alpha modulation and Low Energy logic activated
d52ab64f Adjustements for new entry code: New global variables / functions and loop
593dacd6 Parameters for new entry guidance: Bank and Alpha commanded.
fa8db378 MIDVALUE function: same than clamp but arguments order may be disregarded
5b97baae DPS adjustement for new entry guidance (global variables instead of jsb sim inputs/outputs)
a4061a40 New TAL site: Madris Airport item 10
bdc0e5c4 Merge branch 'development' of ssh://git.code.sf.net/p/fgspaceshuttledev/code
b24cd983 Final flare fine tunned / Adjustement for Qbar filter during final flare to avoid pitchdown near ground
fb408f45 More works on Entry code simulation / Entry guidance code completed(Appendix 1 to 14) and not activated for now
62ef99b5 Removed fast drag modulation for stability purpose
cefae69e Lift acceleration parameter for entry guidance code benchmark
a4612960 Added Paro and Innsbruck for TAEM and final approach scenarios (fictionnal challenges)
d1c91875 Merge /u/dirteat/fgspaceshuttledev/ branch mecoff into development
bda265e0 Gander and Kef coordinates fine tunned for AutoLand
f5d0399e Typo fixed (AUTO/MAN) for MFD in autonomous mode
6bce4330 EGRT targeting routine function completed / Global variables hash for Entry Guidance (Constants, Internal parameters, Output)
5f02b062 45° of bank for OPS6 S-turn / Additional range logic for GRTLS (not activated)
efec9792 Alpha transition boundary set to 320 fps (from TAEM documentations)
92c61a08 Correct pitch error logic for TAEM / Pitch error is based on Nz error from TAEM guidance
5d11ff0d Sign-off auto-launch guidance at MECO based on engine thrust (for manual throttle override)
6283a632 Proper geodetic to rwy frame conversion with matrix formalism (vs. polar coordinates before) // Better guidance accuracy
83cf5416 Entry guidance rework first step: EGRT targeting routine function / geodetic to rwy frame conversion
1c049d51 Easter Island runway 28 slope ( uphill)
9c21c240 Sb opening/closing rated adjusted for Entry update frequency // Better initial conditions for TAEM scenario
edd7b876 Previous Mass Balance values (newer ones need more test during Entry)
e94f6d81 3x3 Matrix computation functions / Geodetic to ECEF frame converter
797233a7 More TAEM rework: Pitch guidance(TGNZC)/ Pitch AP output(TDAP)/ Filters/ Autoland logic up to touchdown (manual rollout)
ff7c872f Approach trainer adjustements to work with last TAEM changes
2ea5e062 More precise threshold coordinates for Autoland in KSC/VBG/EDW/ZZA/FMI/IPC // Runway slope parameter added
960f94c3 OPS 6 TAEM transition slightly adjusted
5282a208 Older TAEM logic jsbsim functions deactivated
1c332acc TAEM pitch rate commanded /TAEM gains
4b31abae Radar altimeter CoG adjustement (Gear extended, CoG is 17 feet above the ground) / Velocity vector adjusted for strong winds and high slopes
0956c8ff Fix some syntax and logical errors on the Eileen stationkeeping script - should improve coarser modes
032c9a52 Stronger coefficient for in HAC radial error correction / Smart flare lower transition (100 feet) to final flare
2c9373c5 Metrics adjusted (MAC and wind incidence) to match Rockwell datas / L/D adjustement factor (10%) below mach 1 to match post test flight analysis / Speedbrake deflection angle adjusted to match in sim deflection vs wind data tunnel SB angle frame
98c1424d Vert traj displays adjusted for latest TAEM Altitude logic
4659645b Typo error for X-range HAC display (inverted logic between PFD and Spec 50)
e1d29333 Fix decimal in Spartan offsets
6709eb9d Add missing texture files for spartan and tdrs
90cbfbc9 Update documentation with new offsets and fix obsoletes
59b1d59b Propadate new offsets to payload functions and main model file
dbeef888 Propagate new offsets and fixture effect on TDRS
6a043e0f Propagate new offsets and fixture effect on Spartan
89a7e743 Propagate new offsets, tune fixture effect on HST
b4bf0230 Tune rms ac model and rms jsbsim computations to match, rms data added in a module
6f12f0d9 Add grapple fixture on TDRS
8dcdc1c6 Update grapple fixture, fix normals, on spartan
4391d876 Resize and adjust grapple fixture to documented 22.5 inches diameter on HST
e086154d Adjust diameter to the end effector at documented 38cm
d84d425d TAEM emulation work: Speedbrake function TGSBC / Deeper TAEM transition logic / HUD cue for IGS intercept and final flare slightly adjusted
b09f5d82 Cd and Cl basic tables based on Rockwell Aerodynamics STS-1 // Ground effect enhanced (function of elevons,AOA,Height/Span)
44e6adc1 Inhibition logic for MEP and STIN downgrade messages
23a55416 Two stage bucket Logic // Boundaries based on TAS // one or two stahe bucket available through mission files
2a8d6fc1 Two stage bucket mission file i-loaded parameters
22a07e7d More work on TAEM emulation: XHAC / GTP / TGCOMP / TGTRAN and TGPHIC functions completed // AutoLand v1 supported
0118a900 TAEM guidance loop replaced by TAEM_TGEXEC for automatic approach scheme
553e2977 Older TAEM functions deactivated / new function for Bank Commanded from TAEM bank function
2f923583 More L/D for Speedbrake (just a rough coefficient, new deeper table in the next commit)
da4549d9 TAEM guidance global variables instead of jsbsim interpolated tables
9dc3d44f More TAEM Logic:TGINIT(Limit parameters IPHASE dependant), TGCOMP (Altitude/Energy/QBar reference functions), Altitude Error function used now for glideslope deviation
2a2a7d17 Merge branch 'development' of ssh://git.code.sf.net/p/fgspaceshuttledev/code
f8b127ac First step of TAEM original logic emulation: Original global variable names // Distance to Runway fine tunned // Final GlideSlope as a function of Weight // Proper Aim Point (7500 feet)
70fb8e3e JSBSim density altitude
81472327 FDM improvements (Basic Cd/Cl, BodyFlaps Cm, Speedbrakes Cl/Cd)
