papers added

_data/pubs/2025.yml

@@ -1,3 +1,12 @@
+- title: "Three Dimensional Waypoint Navigation for Fixed-wing Micro Aerial Vehicles using Integrated Guidance and Control Framework"
+  authors: Harikumar Kandath, Jinraj V Pushpangathan, M Seetharama Bhat
+  venue: 2025 International Conference on Emerging Technology in Autonomous Aerial Vehicles (ETAAV)
+  link: # https://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=11213103
+    url: /publications/2025/Harikumar_Three
+    display: Project Page
+  id: mkrishna
+  featured: 1
+
 - title: "Active Disturbance Rejection based approach for Fault Tolerant Control of a Quadcopter"
   authors: Prachetas P, Dinesh Viswas, Harikumar Kandath, Pooja Agrawal
   venue: 2025 International Conference on Emerging Technology in Autonomous Aerial Vehicles (ETAAV)

_pages/project-pages/2025/Antony_Locally.md

@@ -0,0 +1,28 @@
+---
+layout: project-page-new
+title: "Locally optimal solutions to constraint displacement problems via path-obstacle overlaps"
+authors:
+  - name: Antony Thomas
+    sup: 1
+  - name: Fulvio Mastrogiovanni
+    sup: 2
+  - name: Marco Baglietto
+    sup: 2
+affiliations:
+  - name: Robotics Research Center, IIIT Hyderabad, India
+    link: https://robotics.iiit.ac.in
+    sup: 1
+  - name: University of Genoa
+    link: https://dibris.unige.it/en
+    sup: 2
+permalink: /publications/2025/Antony_Locally/
+abstract: "We present a unified approach for constraint displacement problems in which a robot finds a feasible path by displacing constraints or obstacles. To this end, we propose a two stage process that returns locally optimal obstacle displacements to enable a feasible path for the robot. The first stage proceeds by computing a trajectory through the obstacles while minimizing an appropriate objective function. In the second stage, these obstacles are displaced to make the computed robot trajectory feasible, that is, collision-free. Several examples are provided that successfully demonstrate our approach on two distinct classes of constraint displacement problems"
+#project_page: https://imagine-2-drive.github.io/
+paper: https://www.sciencedirect.com/science/article/pii/S0921889025003483
+#code: https://github.com/Smart-Wheelchair-RRC/CrowdSurfer
+#supplement: https://arxiv.org/abs/2409.16011
+#video: https://iiithydresearch-my.sharepoint.com/personal/shreya_bollimuntha_research_iiit_ac_in/_layouts/15/stream.aspx?id=%2Fpersonal%2Fshreya%5Fbollimuntha%5Fresearch%5Fiiit%5Fac%5Fin%2FDocuments%2FAttachments%2FICRA%5F2025%2Emp4&ga=1&referrer=StreamWebApp%2EWeb&referrerScenario=AddressBarCopied%2Eview%2Edc06e0cd%2Dbfc3%2D4581%2D9eef%2Da7753f1e437a
+#iframe: https://www.youtube.com/embed/BMDCYdxfaXM
+#demo: https://anyloc.github.io/#interactive_demo
+
+---

_pages/project-pages/2025/Prachetas_Active.md

@@ -0,0 +1,32 @@
+---
+layout: project-page-new
+title: "Active Disturbance Rejection based approach for Fault Tolerant Control of a Quadcopter"
+authors:
+  - name: Prachetas P
+    sup: 1
+  - name: Dinesh Viswas
+    sup: 2
+  - name: Harikumar Kandath
+    sup: 3
+  - name: Pooja Agrawal
+    sup: 1
+affiliations:
+  - name: School of Robotics DIAT (DU), Girinagar, Pune
+    link: https://diat.ac.in/school-of-robotics/
+    sup: 1
+  - name: BITS Pilani Goa Campus, Goa, India
+    link: https://www.bits-pilani.ac.in/goa/
+    sup: 2
+  - name: Robotics Research Center, IIIT Hyderabad, India
+    link: https://robotics.iiit.ac.in
+    sup: 3
+permalink: /publications/2025/Prachetas_Active/
+abstract: This paper proposes a fault-tolerant control strat-egy addressing partial-to-complete propeller effectiveness loss through a dual-equilibrium framework. Two operating regimes
+are established based on a fault severity threshold, (i)below- threshold conditions maintain full actuation, (ii)above-threshold operation stabilizes hover dynamics by relinquishing yaw control.
+An Extended State Observer (ESO)-based Active Disturbance Re-jection Control (ADRC) estimates and compensates for combined disturbances, including fault-induced effects and unmodeled
+dynamics. High-fidelity nonlinear simulations demonstrate the framework’s effectiveness in maintaining attitude stabilization and position tracking during fault scenarios. The results vali-date that intentional yaw decoupling in severe faults preserves roll/pitch stability while ESO-ADRC ensures robust disturbance rejection, offering practical fault accommodation for propeller-driven systems
+#project_page: https://reachpranjal.com/sparseloc/
+paper: https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=11213100
+#code:
+#iframe: https://www.youtube.com/embed/PmMC49SNj2k
+---