Algorithms for Walking, Running, Swimming, Flying, and Manipulation

© Russ Tedrake, 2023

Last modified .

How to cite these notes, use annotations, and give feedback.

**Note:** These are working notes used for a course being taught
at MIT. They will be updated throughout the Spring 2023 semester. Lecture videos are available on YouTube.

Previous Chapter | Table of contents | Next Chapter |

The discussion of walking and running robots in Chapter 4 motivated the notion of limit cycle stability. Linear systems are not capable of producing stable limit cycle behavior, so this rich topic is unique to nonlinear systems design and analysis. Furthermore, the tools that are required to design, stabilize, and verify limit cycles will have applicability beyond simple periodic motions.

The first natural question we must ask is, given a system $\dot{\bx} = f(\bx)$, or a control system $\dot{x} = f(\bx,\bu)$, how do we go about finding periodic solutions which may be passively stable, open-loop stable, or stabilizable via closed-loop feedback? It turns out that the trajectory optimization tools that we developed already are very well suited to this task.

I introduced the trajectory optimization tools as means for optimizing a
control trajectory starting from a particular known initial condition. But
the fundamental idea of optimizing over individual trajectories of the
system is useful more broadly. Even for a passive system, we can formulate
the search for a periodic solution as an optimization over trajectories that
satisfy the dynamic constraints and *periodicity constraints*,
$\bx[0] = \bx[N]$: \begin{align*} \find_{\bx[\cdot]} \quad \subjto \quad &
\bx[n+1] = f(\bx[n]), \quad \forall n\in[0, N-1] \\ & \bx[0] = \bx[N].
\end{align*} Certainly we can add control inputs back into the formulation,
too, but let's start with this simple case. Take a moment to think about
the feasible solutions to this problem formulation. Certainly a fixed point
$\bx[n] = \bx^*$ will satisfy the constraints; if we don't want these
solutions to come out of the solver we might need to exclude them with
constraints or add an objective that guides the solver towards the desired
solutions. The other possible solutions are trajectories that are periodic
in exactly $N$ steps. That's pretty restrictive.

We can do better if we use the continuous-time formulations. For instance, in our introduction of direct collocation, we wrote \begin{align*} \min_{\bx[\cdot],\bu[\cdot]} \quad & \ell_f(\bx[N]) + \sum_{n_0}^{N-1} h_n \ell(\bx[n],\bu[n]) \\ \subjto \quad & \dot\bx(t_{c,n}) = f(\bx(t_{c,n}), \bu(t_{c,n})), & \forall n \in [0,N-1] \\ & \bx[0] = \bx_0 \\ & + \text{additional constraints}. \end{align*} But we can also add $h_n$ as decision variables in the optimization (reminder: I recommend setting a lower-bound $h_n \ge h_{min} > 0$). This allows our $N$-step trajectory optimization to scale and shrink time in order to satisfy the periodicity constraint. The result is simple and powerful.

Recall the dynamics of the Van der Pol oscillator given by $$\ddot{q} + \mu (q^2 - 1) \dot{q} + q = 0, \quad \mu>0,$$ which exhibited a stable limit cycle.

Formulate the direct collocation optimization: \begin{align*} \find_{\bx[\cdot],h} \quad \subjto \quad & q[0] = 0, \quad \dot{q}[0] > 0, \\ & \bx[N] = \bx[0], \text{(periodicity constraint)}\\ & \text{collocation dynamic constraints} \\ & 0.01 \le h \le 0.5 \end{align*}

Try it yourself:

As always, make sure that you take a look at the code. Poke around. Try changing some things.

One of the things that you should notice in the code is that I provide an initial guess for the solver. In most of the examples so far I've been able to avoid doing that--the solver takes small random numbers as a default initial guess and solves from there. But for this problem, I found that it was getting stuck in a local minima. Adding the initial guess that the solution moves around a circle in state space was enough.

Recall the important distinction between stability of a trajectory in
time and stability of a limit cycle was that the limit cycle does not
converge in phase -- trajectories near the cycle converge to the cycle,
but trajectories on the cycle may not converge with each other. This is
type of stability, also known as *orbital stability* can be
written as stability to the manifold described by a trajectory $\bx^*(t)$,
\[ \min_\tau || x(t) - x^*(\tau) || \rightarrow 0.\] In the case of limit
cycles, this manifold is a periodic solution with $\bx^*(t+t_{period}) =
\bx^*(t)$. Depending on exactly how that convergence happens, we can define
orbital stability in the sense of Lyapunov, asymptotic orbital stability,
exponential orbital stability, or even finite-time orbital stability.

In order to prove that a system is orbitally stable (locally, over a
region, or globally), or to analyze the region of attraction of a limit
cycle, we can use a Lyapunov function. When we analyzed our simple models of walking and running, we
carried out the analysis on the Poincare map. Indeed, if we can find a
Lyapunov function that proves (i.s.L., asympototic, or exponential)
stability of the discrete Poincare map, then this implies (i.s.L,
asymptotic, or exponential) *orbital* stability of the cycle. But
Lyapunov functions of this form are difficult to verify for a pretty
fundamental reason: we rarely have an analytical expression for the
Poincare map, since it is the result of integrating a nonlinear dynamics
over the cycle.

Instead, we will focus our attention on constructing Lyapunov functions in the full state space, which use the continuous dynamics. In particular, we would like to consider Lyapunov functions which have the form cartooned below; they vanish to zero everywhere along the cycle, and are strictly positive everywhere away from the cycle.

How can we parameterize this class of functions? For arbitrary cycles this could be very difficult in the original coordinates. For simple cycles like in the cartoon, one could imagine using polar coordinates. More generally, we will define a new coordinate system relative to the orbit, with coordinates

- $\tau$ - the phase along the orbit
- $\bx_\perp(\tau)$ - the remaining coordinates, linearly independent from $\tau$.

Given a state $\bx$ in the original coordinates, we must define a smooth mapping $\bx \rightarrow (\tau, \bx_\perp)$ to this new coordinate system. For example, for a simple ring oscillator we might have:

In general, for an $n$-dimensional state space, $\tau$ will always be a scalar, and $\bx_\perp$ will be an $(n-1)$-dimensional vector defining the remaining coordinates relative to $\bx^*(\tau)$. In fact, although we use the notation $\bx_\perp$ the coordinate system need not be strictly orthogonal to the orbit, but must simply beThe value of
this construction for Lyapunov analysis was proposed in

For a dynamical system $\dot\bx = f(\bx)$ with $\bx \in \Re^n$, $f$
continuous, a continuous periodic solution $\bx^*(\tau)$, and a smooth
mapping $\bx \rightarrow (\tau,\bx_\perp)$ where $\bx_\perp$ vanishes on
$\bx^*$, then for some $n-1$ dimensional ball ${\cal B}$ around the
origin, if I can produce a $V(\bx_\perp,\tau)$ such that \begin{gather*}
\forall \tau, V(0,\tau) = 0, \\ \forall \tau, \forall \bx_\perp \in
{\cal B}, \bx_\perp \ne 0, V(\bx_\perp,\tau) > 0, \end{gather*} with
\begin{gather*} \forall \tau, \dot{V}(0,\tau) = 0, \\ \forall \tau,
\forall \bx_\perp \in {\cal B}, \bx_\perp \ne 0, \dot{V}(\bx_\perp,\tau)
< 0, \end{gather*} then the solution $\bx^*(t)$ is *locally orbitally
asymptotically stable*.

Orbital stability in the sense of Lyapunov and exponential orbital stability can also be verified (with $\dot{V}_\perp \le 0$ and $\dot{V}_\perp \le \alpha V_\perp$, respectively).

Perhaps the simplest oscillator is the first-order system which converges to the unit circle. In cartesian coordinates, the dynamics are \begin{align*} \dot{x}_1 =& x_2 -\alpha x_1 \left( 1 - \frac{1}{\sqrt{x_1^2+x_2^2}}\right) \\ \dot{x}_2 =& -x_1 -\alpha x_2 \left( 1 - \frac{1}{\sqrt{x_1^2+x_2^2}}\right), \end{align*} where $\alpha$ is a positive scalar gain.

If we take the transverse coordinates to be the polar coordinates, shifted so that $x_\perp$ is zero on the unit circle, \begin{align*}\tau =& \text{atan2}(-x_2,x_1) \\ x_\perp =& \sqrt{x_1^2+x_2^2}-1, \end{align*} which is valid when $x_\perp>-1$, then the simple transverse dynamics are revealed: \begin{align*} \dot\tau =& 1 \\ \dot{x}_\perp =& -\alpha x_\perp. \end{align*} Taking a Lyapunov candidate $V(x_\perp,\tau) = x_\perp^2$, we can verify that $$\dot{V} = -2 \alpha x_\perp^2 < 0, \quad \forall x_\perp > -1.$$ This demonstrates that the limit cycle is locally asymptotically stable, and furthermore that the invariant open-set $V < 1$ is inside the region of attraction of that limit cycle. In fact, we know that all $x_\perp > -1$ are in the region of attraction that limit cycle, but this is not proven by the Lyapunov argument above.

Let's compare this approach again with the approach that we used in the chapter on walking robots, where we used a Poincaré map analysis to investigate limit cycle stability. In transverse coordinates approach, there is an additional burden to construct the coordinate system along the entire trajectory, instead of only at a single surface of section. In fact, the transverse coordinates approach is sometimes referred to as a "moving Poincaré section". Again, the reward for this extra work is that we can check a condition that only involves the instantaneous dynamics, $f(\bx)$, as opposed to having to integrate the dynamics over an entire cycle to generate the discrete Poincaré map, $\bx_p[n+1] = P(\bx_p[n])$. As we will see below, this approach will also be more compatible with designing continuous feedback controller that stabilize the limit cycle.

In the case of Lyapunov analysis around a fixed point, there was an important special case: for stable linear systems, we actually have a recipe for constructing a Lyapunov function. As a result, for nonlinear systems, we often found it convenient to begin our search by linearizing around the fixed point and using the Lyapunov candidate for the linear system as an initial guess. That same approach can be extended to limit cycle analysis.

In particular, let us make a linear approximation of the transverse
dynamics: $$\dot{\bx}_\perp = f_\perp(\bx_\perp, \tau) \approx
\pd{f_\perp}{\bx_\perp} \bx_\perp = \bA_\perp(\tau)\bx_\perp.$$ Note that
I've assumed that $\bx_\perp$ is zero on the nominal trajectory, so don't
need the additional notation of working in the error coordinates here.
Remember that $\tau$ is the phase along the trajectory, but
*time-varying* linear system $\dot\bx_\perp = \bA_\perp(t)
\bx_\perp$ implies local exponential orbital stability of the original
system. In particular, if this transverse linear system is periodic and
orbitally stable, then for each $\bQ=\bQ^T \succ 0$, there exists a
unique positive definite solution to the periodic Riccati equation:
\begin{gather*} V(\bx_\perp, \tau) = \bx_\perp^T {\bf P}(\tau) \bx_\perp,
\qquad {\bf P}^T(\tau) = {\bf P}(\tau), \quad {\bf P}(\tau + t_{period})
= {\bf P}(\tau), \\ -\dot{\bf P}(\tau) = {\bf P}(\tau) \bA(\tau) +
\bA(\tau){\bf P}^T(\tau) + \bQ, \qquad \bQ=\bQ^T\succ 0. \end{gather*}
There is a surprisingly rich literature on the numerical methods for
finding the periodic solutions to these Lyapunov (and corresponding
Riccati) equations. In practice, for every problem I've ever tried, I've
simply integrated the equations backwards in time until the integration
converges to a periodic solution (this is not guaranteed to work, but
almost always does).

This is very powerful. It gives us a general way to construct a Lyapunov candidate that certifies local stability of the cycle, and which can be used as a candidate for nonlinear Lyapunov analysis.

Coming soon. If you are interested, see

Many of the tools we've developed for stabilization of fixed points or stabilization of trajectories can be adapted to this new setting. When we discussed control for the spring-loaded inverted pendulum model, we considered discrete control decisions, made once per cycle, which could stabilize the discrete Poincare map, $\bx_p[n+1] = f_p(\bx_p[n], \bu[n]),$ with $\bu[n]$ the once-per-cycle decisions. While it's possible to get the local linear approximations of this map using our adjoint methods, remember that we rarely have an analytical expression for the nonlinear $f_p$.

How limiting is it to restrict ourselves to once-per-cycle decisions? Of course we can improve performance in general with continuous feedback. But there are also some cases where once-per-cycle decisions feel quite reasonable. Foot placement for legged robots is a good example -- once we've chosen a foot placement we might make minor corrections just before we place the foot, but rarely change that decision once the foot is on the ground; once per footstep seems like a reasonable approximation. Another good example is flapping flight: here the wing beat cycle times can be much faster than the dynamic timescales of the center of mass, and changing the parameters of the wing stroke one per flap seems pretty reasonable.

But the tools we've developed above also give us the machinery we need to consider continuous feedback throughout the trajectory. Let's look at a few important formulations.

It turns out many of our simple walking models -- particularly ones with a point foot that are derived in the minimal coordinates -- are only short one actuator (between the foot and the ground). One can represent even fairly complex robots this way; much of the theory that I'll elude to here was originally developed by Jessy Grizzle and his group in the context of the bipedal robot RABBIT. Jessy's key observation was that limit cycle stability is effectively stability in $n-1$ degrees of freedom, and you can often achieve it easily with $n-1$ actuators -- he called this line of work "Hybrid Zero Dynamics" (HZD). We'll deal with the "hybrid" part of that in the next chapter, but here is a simple example to illustrate the "zero dynamics" concept. [Coming soon...]

Stabilizing the zero dynamics is synonymous with achieving orbital stability. Interestingly, it doesn't actually guarantee that you will go around the limit cycle. One "feature" of the HZD walkers is that you can actually stand in front of them and stop their forward progress with your hand -- the control system will continue to act, maintaining itself on the cycle, but progress along the cycle has stopped. In some of the robots you could even push them backwards and they would move through the same walking cycle in reverse. If one wants to certify that forward progress will be achieved, then the tasks is reduced to inspecting the one-dimensional dynamics of the phase variable along the cycle.

The notion of "zero dynamics" is certainly not restricted to systems with underactuation of degree one. In general, we can easily stabilize a manifold of dimension $m$ with $m$ actuators (we saw this in the section on task-space partial feedback linearization), and if being on that manifold is sufficient to achieve our task, or if we can certify that the resulting dynamics on the manifold are sufficient for our task, then life is good. But in the "underactuation degree one" case, the manifold under study is a trajectory/orbit, and the tools from this chapter are immediately applicable.

Another natural approach to stabilizing a cycle uses the transverse
linearization. In particular, for a nominal (control) trajectory,
$[\bx_0(t), \bu_0(t)],$ with $\dot{\bx}_0 = f(\bx_0, \bu_0)$, we can
approximate the transverse dynamics: $$\dot{\bx}_\perp =
f_\perp(\bx_\perp, \tau, \bu) \approx \pd{f_\perp}{\bx_\perp} \bx_\perp +
\pd{f_\perp}{\bu}(\bu - \bu_0(\tau)) = \bA_\perp(\tau)\bx_\perp +
\bB_\perp(\tau) \bar{\bu}.$$ *orbital* stabilization of the original system.

Let's take a minute to appreciate the difference between this approach and time-varying LQR in the full coordinates. Of course, the behavior is quite different: time-varying LQR in the full coordinates will try to slow down or speed up to keep time with the nominal trajectory, where this controller makes no attempt to stabilize the phase variable. You might think you could design the original time-varying controller, $\bar\bu = \bK(t)\bar\bx,$ and just "project to the closest time" during execution (e.g. find the time $t = \argmin_\tau |\bx - \bx_0(\tau)|)$ and use the feedback corresponding to that time. But this projection is not guaranteed to be safe; you can find systems that are stabilizable by the transverse linearization are unstable in closed-loop using a feedback based on this projection.

Coming soon...

But there is an even more important reason to like the transverse LQR approach. If orbital stability is all you need, then this is a better formulation of the problem because you are asking for less. As we've just discussed with hybrid zero-dynamics, stabilizing $m$ degrees of freedom with $m$ actuators is potentially very different than stabilizing $m+1$ degrees of freedom. In the transverse formulation, we are asking LQR to minimize the cost only in the transverse coordinates (it is mathematically equivalent to designing a cost function in the full coordinates that is zero in the direction of the nominal trajectory). In practice, this can result is much smaller cost-to-go matrices, ${\bf S}(t)$, and smaller feedback gains, $\bK(t)$. For underactuated systems, this difference can be dramatic.

The observation that orbital stabilization of a trajectory can ask much less of your underactuated control system (and lead to smaller LQR feedback gains), is quite powerful. It is not limited to stabilizing periodic motions. If your aim is to stabilize a non-periodic path through state-space, but do not actually care about the timing, then formulating your stabilization can be a very good choice. You can find examples where a system is stabilizable in the transverse coordinates, but not in the full coordinates.

Coming soon...

Take care, though, as the converse can also be true: it's possible
that a system could be stabilizable in the full coordinates but
*not* in some transverse coordinates; if you choose those
coordinates badly.

Consider a trajectory with $u(t) = 1$ (from any initial condition) for the double integrator. We can certainly stablize this trajectory in the full coordinates using LQR. Technically, one can choose transverse coordinates $\tau = \dot{q},$ and $x_\perp = q.$ Clearly $x_\perp$ is transverse to the nominal trajectory everywhere. But this transverse linearization is also clearly not stabilizable. It's a bad choice!

The general approach to designing the transverse coordinates

- "Converse {L}yapunov functions for exponentially stable periodic orbits", Systems & Control Letters, vol. 23, no. 1, pp. 27 -- 34, 1994. ,
- "Can We Make a Robot Ballerina Perform a Pirouette? Orbital Stabilization of Periodic Motions of Underactuated Mechanical Systems", Annual Reviews in Control, vol. 32, no. 2, pp. 200--211, Dec, 2008. ,
- "Regions of Attraction for Hybrid Limit Cycles of Walking Robots", Proceedings of the 18th IFAC World Congress, extended version available online: arXiv:1010.2247 [math.OC], 2011. ,
- "Transverse Dynamics and Regions of Stability for Nonlinear Hybrid Limit Cycles", Proceedings of the 18th IFAC World Congress, extended version available online: arXiv:1010.2241 [math.OC], Aug-Sep, 2011. ,

Previous Chapter | Table of contents | Next Chapter |