Removed "introduction" and "conclusion" from the TOC

phd-thesis.org

@@ -320,6 +320,7 @@ The conceptual design of the Nano Active Stabilization System (NASS) follows a m
 #+name: fig:chapter1_overview
 #+caption: Overview of the conceptual design development. The approach evolves from simplified analytical models to a multi-body model tuned from experimental modal analysis. It is concluded by closed-loop simulations of tomography experiments, validating the conceptual design.
 #+attr_org: :width 800px
+#+attr_latex: :options [h!tbp]
 #+attr_latex: :width \linewidth
 [[file:figs/chapter1_overview.png]]
 
@@ -1554,6 +1555,9 @@ Having some flexibility between the measurement point and the point of interest
 Therefore, it is important to take special care when designing sampling environments, especially if a soft nano-hexapod is used.
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 <<sec:uniaxial_conclusion>>
 
 # TODO - Make a table summarizing the findings
@@ -2583,6 +2587,9 @@ Conclusions are similar than those of the uniaxial (non-rotating) model:
 #+end_figure
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 
 In this study, the gyroscopic effects induced by the spindle's rotation have been studied using a simplified model (Section\nbsp{}ref:sec:rotating_system_description).
 Decentralized acrlong:iff with pure integrators was shown to be unstable when applied to rotating platforms (Section\nbsp{}ref:sec:rotating_iff_pure_int).
@@ -3175,6 +3182,9 @@ This can be seen in Figure\nbsp{}ref:fig:modal_comp_acc_frf_modal_3 that shows t
 #+end_figure
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 <<sec:modal_conclusion>>
 
 In this study, a modal analysis of the micro-station was performed.
@@ -4007,6 +4017,9 @@ A similar error amplitude was observed, thus indicating that the multi-body mode
 [[file:figs/ustation_errors_model_dy_vertical.png]]
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 <<sec:ustation_conclusion>>
 
 In this study, a multi-body model of the micro-station was developed.
@@ -4985,6 +4998,9 @@ The collocated nature of the force sensors ensures stability despite strong coup
 The outer loop implements High Authority Control, enabling precise positioning of the mobile platform.
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 <<sec:nhexa_conclusion>>
 
 After evaluating various architectures, the Stewart platform was selected for the active platform.
@@ -5007,7 +5023,7 @@ This study establishes the theoretical framework necessary for the subsequent de
 
 ** Validation of the Concept
 <<sec:nass>>
-*** Introduction
+*** Introduction                                                    :ignore:
 
 The previous chapters have established crucial foundational elements for the development of the Nano Active Stabilization System (NASS).
 The uniaxial model study demonstrated that very stiff nano-hexapod configurations should be avoided due to their high coupling with the micro-station dynamics.
@@ -5506,6 +5522,9 @@ For higher mass configurations, rotational velocities are expected to be below 3
 #+end_figure
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: t
+:END:
 <<sec:nass_conclusion>>
 
 The development and analysis presented in this chapter have successfully validated the Nano Active Stabilization System concept, marking the completion of the conceptual design phase.
@@ -6531,6 +6550,9 @@ This specification will guide the design of the flexible joints.
 # TODO - Add link to section
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: notoc
+:END:
 <<sec:detail_kinematics_conclusion>>
 
 This chapter has explored the optimization of the nano-hexapod geometry for the Nano Active Stabilization System (NASS).
@@ -7309,6 +7331,9 @@ While additional degrees of freedom could potentially capture more dynamic featu
 #+end_figure
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: notoc
+:END:
 <<sec:detail_fem_conclusion>>
 
 In this chapter, the methodology of combining finite element analysis with multi-body modeling has been demonstrated and validated, proving particularly valuable for the detailed design of nano-hexapod components.
@@ -8821,6 +8846,9 @@ The control architecture has been presented for SISO systems, but can be applied
 It will be experimentally validated with the NASS during the experimental phase.
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: notoc
+:END:
 <<sec:detail_control_conclusion>>
 
 In order to optimize the control of the Nano Active Stabilization System, several aspects of control theory were studied.
@@ -9399,6 +9427,9 @@ This confirms that the selected instrumentation, with its measured noise charact
 [[file:figs/detail_instrumentation_cl_noise_budget.png]]
 
 *** Conclusion
+:PROPERTIES:
+:UNNUMBERED: notoc
+:END:
 <<sec:detail_instrumentation_conclusion>>
 
 This section has presented a comprehensive approach to the selection and characterization of instrumentation for the nano active stabilization system.
@@ -9492,6 +9523,7 @@ The HAC-LAC control architecture is implemented and tested under various experim
 #+name: fig:chapter3_overview
 #+caption: Overview of the Experimental validation phase. The actuators and flexible joints and individual tested and then integrated into the struts. The Nano-hexapod is then mounted and the complete system is validated on the ID31 beamline.
 #+attr_org: :width 800px
+#+attr_latex: :options [h!tbp]
 #+attr_latex: :width \linewidth
 [[file:figs/chapter3_overview.png]]
 
@@ -13025,11 +13057,6 @@ With the implementation of an accurate online metrology system, the NASS will be
 * TODO Conclusion and Future Work
 <<chap:conclusion>>
 
-* Appendix                                                   :noexport:ignore:
-#+latex: \appendix
-
-* Mathematical Tools for Mechatronics                               :noexport:
-* Stewart Platform - Kinematics                                     :noexport:
 * Bibliography                                                        :ignore:
 #+latex: \printbibliography[heading=bibintoc,title={Bibliography}]